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Robert H. Goddard
Robert H. Goddard
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Robert Hutchings Goddard (October 5, 1882 – August 10, 1945)[1] was an American physicist, inventor, and engineer credited with creating and building the world's first liquid-fueled rocket, which was successfully launched on March 16, 1926.[2] By 1915 his pioneering work had dramatically improved the efficiency of the solid-fueled rocket, signaling the era of the modern rocket and innovation. He and his team launched 34 rockets between 1926 and 1941, achieving altitudes as high as 2.6 km (1.6 mi) and speeds as fast as 885 km/h (550 mph).[3]

Key Information

Goddard's work as both theorist and engineer anticipated many of the developments that would make spaceflight possible.[4] He has been called the man who ushered in the Space Age.[5]: xiii  Two of Goddard's 214 patented inventions, a multi-stage rocket (1914), and a liquid-fuel rocket (1914), were important milestones toward spaceflight.[6] His 1919 monograph A Method of Reaching Extreme Altitudes is considered one of the classic texts of 20th-century rocket science.[7][8] Goddard successfully pioneered modern methods such as two-axis control (gyroscopes and steerable thrust) to allow rockets to control their flight effectively.

Although his work in the field was revolutionary, Goddard received little public or financial support for his research and development work.[9]: 92, 93  He was a shy person, and rocket research was not considered a suitable pursuit for a physics professor.[10]: 12  The press and other scientists ridiculed his theories of spaceflight. As a result, he became protective of his privacy and his work.

Years after his death, at the dawn of the Space Age, Goddard came to be recognized as one of the founding fathers of modern rocketry, along with Robert Esnault-Pelterie, Konstantin Tsiolkovsky and Hermann Oberth.[11][12][13] He not only recognized early on the potential of rockets for atmospheric research, ballistic missiles and space travel, but also was the first to scientifically study, design, construct and fly the precursory rockets needed to eventually implement those ideas.[14]

NASA's Goddard Space Flight Center was named in Goddard's honor in 1959. He was also inducted into the International Aerospace Hall of Fame and National Aviation Hall of Fame in 1966, and the International Space Hall of Fame in 1976.[15]

Early life and inspiration

[edit]

Goddard was born in Worcester, Massachusetts, to Nahum Danford Goddard (1859–1928) and Fannie Louise Hoyt (1864–1920). Robert was their only child to survive; a younger son, Richard Henry, was born with a spinal deformity and died before his first birthday. His father Nahum was employed by manufacturers and invented several useful tools.[16] Goddard had English paternal family roots in New England with William Goddard (1628–91) a London grocer who settled in Watertown, Massachusetts, in 1666. This line of Goddards were previously called Goddardville.[17] On his maternal side he was descended from John Hoyt and other settlers of Massachusetts in the late 1600s.[18][19] Shortly after his birth, the family moved to Boston. With a curiosity about nature, he studied the heavens using a telescope from his father and observed the birds flying. Essentially a country boy, he loved the outdoors and hiking with his father on trips to Worcester and became an excellent marksman with a rifle.[20]: 63, 64  In 1898, his mother contracted tuberculosis and they moved back to Worcester for the clear air. On Sundays, the family attended the Episcopal church, and Robert sang in the choir.[16]: 16 

Childhood experiments

[edit]

With the electrification of American cities in the 1880s, the young Goddard became interested in science—specifically, engineering and technology. When his father showed him how to generate static electricity on the family's carpet, the five-year-old's imagination was sparked. Robert experimented, believing he could jump higher if the zinc from a battery could be charged by scuffing his feet on the gravel walk. But, holding the zinc, he could jump no higher than usual.[16]: 15 [21] Goddard halted the experiments after a warning from his mother that if he succeeded, he could "go sailing away and might not be able to come back."[22]: 9  He experimented with chemicals and created a cloud of smoke and an explosion in the house.[20]: 64  Goddard's father encouraged Robert's scientific interest further by providing him with a telescope, a microscope, and a subscription to Scientific American.[22]: 10  Robert developed a fascination with flight, first with kites and then with balloons. He became a thorough diarist and documenter of his work—a skill that would greatly benefit his later career. These interests merged at age 16, when Goddard attempted to construct a balloon out of aluminum, shaping the raw metal in his home workshop, and filling it with hydrogen. After nearly five weeks of methodical, documented efforts, he finally abandoned the project, remarking, "... balloon will not go up. ... Aluminum is too heavy. Failior [sic] crowns enterprise." However, the lesson of this failure did not restrain Goddard's growing determination and confidence in his work.[16]: 21  He wrote in 1927, "I imagine an innate interest in mechanical things was inherited from a number of ancestors who were machinists."[23]: 7 

Cherry tree dream

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He became interested in space at the age of 16 when he read H. G. Wells' newly published novel The War of the Worlds, in which England is invaded by an alien species from Mars. His dedication to pursuing space flight became fixed on October 19, 1899. The 17-year-old Goddard climbed a cherry tree to cut off dead limbs. He was transfixed by the sky, and his imagination grew. He later wrote:

On this day I climbed a tall cherry tree at the back of the barn ... and as I looked toward the fields at the east, I imagined how wonderful it would be to make some device which had even the possibility of ascending to Mars, and how it would look on a small scale, if sent up from the meadow at my feet. I have several photographs of the tree, taken since, with the little ladder I made to climb it, leaning against it.

It seemed to me then that a weight whirling around a horizontal shaft, moving more rapidly above than below, could furnish lift by virtue of the greater centrifugal force at the top of the path.

I was a different boy when I descended the tree from when I ascended. Existence at last seemed very purposive.[16]: 26 [24]

For the rest of his life, he observed October 19 as "Anniversary Day", a private commemoration of the day of his greatest inspiration.

Education and early studies

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The young Goddard was a thin and frail boy, almost always in fragile health. He suffered from stomach problems, pleurisy, colds, and bronchitis, and he fell two years behind his classmates. He became a voracious reader, regularly visiting the local public library to borrow books on the physical sciences.[16]: 16, 19 

Aerodynamics and motion

[edit]

Goddard's interest in aerodynamics led him to study some of Samuel Langley's scientific papers in the periodical Smithsonian. In these papers, Langley wrote that birds flap their wings with different force on each side to turn in the air. Inspired by these articles, the teenage Goddard watched swallows and chimney swifts from the porch of his home, noting how subtly the birds moved their wings to control their flight. He noted how remarkably the birds controlled their flight with their tail feathers, which he called the birds' equivalent of ailerons. He took exception to some of Langley's conclusions and in 1901 wrote a letter to St. Nicholas magazine[22]: 5  with his own ideas. The editor of St. Nicholas declined to publish Goddard's letter, remarking that birds fly with a certain amount of intelligence and that "machines will not act with such intelligence."[16]: 31  Goddard disagreed, believing that a man could control a flying machine with his own intelligence.

Around this time, Goddard read Newton's Principia Mathematica, and found that Newton's third law of motion applied to motion in space. He wrote later about his own tests of the law:

I began to realize that there might be something after all to Newton's Laws. The Third Law was accordingly tested, both with devices suspended by rubber bands and by devices on floats, in the little brook back of the barn, and the said law was verified conclusively. It made me realize that if a way to navigate space were to be discovered, or invented, it would be the result of a knowledge of physics and mathematics.[16]: 32 

Academics

[edit]

As his health improved, Goddard continued his formal schooling as a 19-year-old sophomore at South High in Worcester in 1901. He excelled in his coursework, and his peers twice elected him class president. Making up for lost time, he studied books on mathematics, astronomy, mechanics and composition from the school library.[16]: 32  At his graduation ceremony in 1904, he gave his class oration as valedictorian. In his speech, entitled "On Taking Things for Granted", Goddard included a section that would become emblematic of his life:

[J]ust as in the sciences we have learned that we are too ignorant to safely pronounce anything impossible, so for the individual, since we cannot know just what are his limitations, we can hardly say with certainty that anything is necessarily within or beyond his grasp. Each must remember that no one can predict to what heights of wealth, fame, or usefulness he may rise until he has honestly endeavored, and he should derive courage from the fact that all sciences have been, at some time, in the same condition as he, and that it has often proved true that the dream of yesterday is the hope of today and the reality of tomorrow.[22]: 19 

Goddard enrolled at Worcester Polytechnic Institute in 1904.[16]: 41  He quickly impressed the head of the physics department, A. Wilmer Duff, with his thirst for knowledge, and Duff took him on as a laboratory assistant and tutor.[16]: 42  At WPI, Goddard joined the Sigma Alpha Epsilon fraternity and began a long courtship with high school classmate Miriam Olmstead, an honor student who had graduated with him as salutatorian. Eventually, she and Goddard were engaged, but they drifted apart and ended the engagement around 1909.[16]: 51 

Goddard at Clark University

Goddard received his B.S. degree in physics from Worcester Polytechnic in 1908,[16]: 50  and after serving there for a year as an instructor in physics, he began his graduate studies at Clark University in Worcester in the fall of 1909.[25] While studying at Clark, Goddard continued working in Salisbury Labs at WPI and anecdotally caused a damaging explosion, whereupon his work was moved to the Magnetic Lab (today called Skull Tomb).[26]

Goddard received his M.A. degree in physics from Clark University in 1910, and then stayed at Clark to complete his Ph.D. in physics in 1911. He spent another year at Clark as an honorary fellow in physics, and in 1912 he accepted a research fellowship at Princeton University's Palmer Physical Laboratory.[16]: 56–58 

First scientific writings

[edit]

The high-school student summed up his ideas on space travel in a proposed article, "The Navigation of Space," which he submitted to the Popular Science News. The journal's editor returned it, saying that they could not use it "in the near future."[16]: 34 

While still an undergraduate, Goddard wrote a paper proposing a method for balancing airplanes using gyro-stabilization. He submitted the idea to Scientific American, which published the paper in 1907. Goddard later wrote in his diaries that he believed his paper was the first proposal of a way to automatically stabilize aircraft in flight.[16]: 50  His proposal came around the same time as other scientists were making breakthroughs in developing functional gyroscopes.

While studying physics at WPI, ideas came to Goddard's mind that sometimes seemed impossible, but he was compelled to record them for future investigation. He wrote that "there was something inside which simply would not stop working." He purchased some cloth-covered notebooks and began filling them with a variety of thoughts, mostly concerning his dream of space travel.[23]: 11–13  He considered centrifugal force, radio waves, magnetic reaction, solar energy, atomic energy, ion or electrostatic propulsion and other methods to reach space. After experimenting with solid-fuel rockets he was convinced by 1909 that chemical-propellant engines were the answer.[10]: 11–12  A particularly complex concept was set down in June 1908: Sending a camera around distant planets, guided by measurements of gravity along the trajectory, and returning to earth.[23]: 14 

His first writing on the possibility of a liquid-fueled rocket came on February 2, 1909. Goddard had begun to study ways of increasing a rocket's efficiency using methods differing from conventional solid-fuel rockets. He wrote in his notebook about using liquid hydrogen as a fuel with liquid oxygen as the oxidizer. He believed that 50-percent efficiency could be achieved with these liquid propellants (i.e., half of the heat energy of combustion converted to the kinetic energy of the exhaust gases).[16]: 55 

First patents

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In the decades around 1910, radio was a new technology, fertile for innovation. In 1912, while working at Princeton University, Goddard investigated the effects of radio waves on insulators.[27] In order to generate radio-frequency power, he invented a vacuum tube with a beam deflection[28] that operated like a cathode-ray oscillator tube. His patent on this tube, which predated that of Lee De Forest, became central in the suit between Arthur A. Collins, whose small company made radio transmitter tubes, and AT&T and RCA over his use of vacuum tube technology. Goddard accepted only a consultant's fee from Collins when the suit was dropped. Eventually, the two big companies allowed the country's growing electronics industry to use the De Forest patents freely.[29]

Rocket math

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By 1912 he had in his spare time, using calculus, developed the mathematics which allowed him to calculate the position and velocity of a rocket in vertical flight, given the weight of the rocket and weight of the propellant and the velocity (with respect to the rocket frame) of the exhaust gases. In effect he had independently developed the Tsiolkovsky rocket equation published a decade earlier in Russia. Tsiolkovsky, however, did not account for gravity nor drag. For vertical flight from the surface of Earth Goddard included in his differential equation the effects of gravity and aerodynamic drag.[23]: 136  He wrote: "An approximate method was found necessary ... in order to avoid an unsolved problem in the calculus of variations. The solution that was obtained revealed the fact that surprisingly small initial masses would be necessary ... provided the gases were ejected from the rocket at a high velocity, and also provided that most of the rocket consisted of propellant material."[23]: 338–9 

His first goal was to build a sounding rocket with which to study the atmosphere. Not only would such investigation aid meteorology, but it was necessary to determine temperature, density and wind speed as functions of altitude in order to design efficient space launch vehicles. He was very reluctant to admit that his ultimate goal was, in fact, to develop a vehicle for flights into space, since most scientists, especially in the United States, did not consider such a goal to be a realistic or practical scientific pursuit, nor was the public yet ready to give serious consideration to such ideas. Later, in 1933, Goddard said that "[I]n no case must we allow ourselves to be deterred from the achievement of space travel, test by test and step by step, until one day we succeed, cost what it may."[20]: 65, 67, 74, 101 

Illness

[edit]

In early 1913, Goddard became seriously ill with tuberculosis and had to leave his position at Princeton. He then returned to Worcester, where he began a prolonged process of recovery at home. His doctors did not expect him to live. He decided he should spend time outside in the fresh air and walk for exercise, and he gradually improved.[16]: 61–64  When his nurse discovered some of his notes in his bed, he kept them, arguing, "I have to live to do this work."[20]: 66 

It was during this period of recuperation, however, that Goddard began to produce some of his most important work. As his symptoms subsided, he allowed himself to work an hour per day with his notes made at Princeton. He was afraid that nobody would be able to read his scribbling should he succumb.[16]: 63 

Foundational patents

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In the technological and manufacturing atmosphere of Worcester, patents were considered essential, not only to protect original work but as documentation of first discovery. He began to see the importance of his ideas as intellectual property, and thus began to secure those ideas before someone else did—and he would have to pay to use them. In May 1913, he wrote descriptions concerning his first rocket patent applications. His father brought them to a patent lawyer in Worcester who helped him to refine his ideas for consideration. Goddard's first patent application was submitted in October 1913.[16]: 63–70 

In 1914, his first two landmark patents were accepted and registered. The first, U.S. patent 1,102,653, described a multi-stage rocket fueled with a solid "explosive material." The second, U.S. patent 1,103,503, described a rocket fueled with a solid fuel (explosive material) or with liquid propellants (gasoline and liquid nitrous oxide). The two patents would eventually become important milestones in the history of rocketry.[30][31] Overall, 214 patents were published, some posthumously by his wife.

Early rocketry research

[edit]
Video clips of Goddard's launches and other events in his life

In the fall of 1914 Goddard's health had improved, and he accepted a part-time position as an instructor and research fellow at Clark University.[16]: 73  His position at Clark allowed him to further his rocketry research. He ordered numerous supplies that could be used to build rocket prototypes for launch and spent much of 1915 in preparation for his first tests. Goddard's first test launch of a powder rocket came on an early evening in 1915 following his daytime classes at Clark.[16]: 74  The launch was loud and bright enough to arouse the alarm of the campus janitor, and Goddard had to reassure him that his experiments, while being serious study, were also quite harmless. After this incident Goddard took his experiments inside the physics lab in order to limit any disturbance.

At the Clark physics lab, Goddard conducted static tests of powder rockets to measure their thrust and efficiency. He found his earlier estimates to be verified; powder rockets were converting only about two percent of the thermal energy in their fuel into thrust and kinetic energy. At this point he applied de Laval nozzles, which were generally used with steam turbine engines, and these greatly improved efficiency. (Of the several definitions of rocket efficiency, Goddard measured in his laboratory what is today called the internal efficiency of the engine: the ratio of the kinetic energy of the exhaust gases to the available thermal energy of combustion, expressed as a percentage.)[23]: 130  By mid-summer of 1915 Goddard had obtained an average efficiency of 40 percent with a nozzle exit velocity of 6,728 feet (2,051 meters) per second.[16]: 75  Connecting a combustion chamber full of gunpowder to various converging-diverging expansion (de Laval) nozzles, Goddard was able in static tests to achieve engine efficiencies of more than 63% and exhaust velocities of over 7,000 feet (2,134 meters) per second.[16]: 78 

Few would recognize it at the time, but this little engine was a major breakthrough. These experiments suggested that rockets could be made powerful enough to escape Earth and travel into space. This engine and subsequent experiments sponsored by the Smithsonian Institution were the beginning of modern rocketry and, ultimately, space exploration.[32] Goddard realized, however, that it would take the more efficient liquid propellants to reach space.[33]

Later that year, Goddard designed an elaborate experiment at the Clark physics lab and proved that a rocket would perform in a vacuum such as that in space. He believed it would, but many other scientists were not yet convinced.[34] His experiment demonstrated that a rocket's performance actually decreases under atmospheric pressure.

In September 1906 he wrote in his notebook about using the repulsion of electrically charged particles (ions) to produce thrust.[23]: 13  From 1916 to 1917, Goddard built and tested the first known experimental ion thrusters, which he thought might be used for propulsion in the near-vacuum conditions of outer space. The small glass engines he built were tested at atmospheric pressure, where they generated a stream of ionized air.[35]

Smithsonian Institution sponsorship

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By 1916, the cost of Goddard's rocket research had become too great for his modest teaching salary to bear.[16]: 76  He began to solicit potential sponsors for financial assistance, beginning with the Smithsonian Institution, the National Geographic Society, and the Aero Club of America.

In his letter to the Smithsonian in September 1916, Goddard claimed he had achieved a 63% efficiency and a nozzle velocity of almost 2438 meters per second. With these performance levels, he believed a rocket could vertically lift a weight of 1 lb (0.45 kg) to a height of 232 miles (373 km) with an initial launch weight of only 89.6 lbs (40.64 kg).[36] (Earth's atmosphere can be considered to end at 80 to 100 miles (130 to 160 km) altitude, where its drag effect on orbiting satellites becomes minimal.)

The Smithsonian was interested and asked Goddard to elaborate upon his initial inquiry. Goddard responded with a detailed manuscript he had already prepared, entitled A Method of Reaching Extreme Altitudes.[16]: 79 

In January 1917, the Smithsonian agreed to provide Goddard with a five-year grant totaling US$5000.[16]: 84  Afterward, Clark was able to contribute US$3500 and the use of their physics lab to the project. Worcester Polytechnic Institute also allowed him to use its abandoned Magnetics Laboratory on the edge of campus during this time, as a safe place for testing.[16]: 85  WPI also made some parts in their machine shop.

Goddard's fellow Clark scientists were astonished at the unusually large Smithsonian grant for rocket research, which they thought was not real science.[16]: 85  Decades later, rocket scientists who knew how much it cost to research and develop rockets said that he had received little financial support.[37][38]

Two years later, at the insistence of Arthur G. Webster, the world-renowned head of Clark's physics department, Goddard arranged for the Smithsonian to publish the paper, A Method..., which documented his work.[16]: 102 

While at Clark University, Goddard did research into solar power using a parabolic dish to concentrate the Sun's rays on a machined piece of quartz, that was sprayed with mercury, which then heated water and drove an electric generator. Goddard believed his invention had overcome all the obstacles that had previously defeated other scientists and inventors, and he had his findings published in the November 1929 issue of Popular Science.[39]

Goddard's military rocket

[edit]
Goddard loading a rocket in 1918

Not all of Goddard's early work was geared toward space travel. As the United States entered World War I in 1917, the country's universities began to lend their services to the war effort. Goddard believed his rocket research could be applied to many different military applications, including mobile artillery, field weapons and naval torpedoes. He made proposals to the Navy and Army. No record exists in his papers of any interest by the Navy to Goddard's inquiry. However, Army Ordnance was quite interested, and Goddard met several times with Army personnel.[16]: 89 

During this time, Goddard was also contacted, in early 1918, by a civilian industrialist in Worcester about the possibility of manufacturing rockets for the military. However, as the businessman's enthusiasm grew, so did Goddard's suspicion. Talks eventually broke down as Goddard began to fear his work might be appropriated by the business. However, an Army Signal Corps officer tried to make Goddard cooperate, but he was called off by General George Squier of the Signal Corps who had been contacted by Secretary of the Smithsonian Institution, Charles Walcott.[16]: 89–91  Goddard became leery of working with corporations and was careful to secure patents to "protect his ideas."[16]: 152  These events led to the Signal Corps sponsorship of Goddard's work during World War I.[16]: 91 

Goddard proposed to the Army an idea for a tube-based rocket launcher as a light infantry weapon. The launcher concept became the precursor to the bazooka.[16]: 92  The rocket-powered, recoil-free weapon was the brainchild of Goddard as a side project (under Army contract) of his work on rocket propulsion. Goddard, during his tenure at Clark University, and working at Mount Wilson Observatory for security reasons, designed the tube-fired rocket for military use during World War I. He and his co-worker Clarence N. Hickman successfully demonstrated his rocket to the U.S. Army Signal Corps at Aberdeen Proving Ground, Maryland, on November 6, 1918, using two music stands for a launch platform. The Army was impressed, but the Compiègne Armistice was signed only five days later, and further development was discontinued as World War I ended.[40]

The delay in the development of the bazooka and other weapons was a result of the long recovery period required from Goddard's serious bout with tuberculosis. Goddard continued to be a part-time consultant to the U.S. Government at Indian Head, Maryland,[16]: 121  until 1923, but his focus had turned to other research involving rocket propulsion, including work with liquid fuels and liquid oxygen.

Later, the former Clark University researcher Clarence N. Hickman and Army officers Col. Leslie Skinner and Lt. Edward Uhl continued Goddard's work on the bazooka. A shaped-charge warhead was attached to the rocket, leading to the tank-killing weapon used in World War II and to many other powerful rocket weapons.[16]: 305 

A Method of Reaching Extreme Altitudes

[edit]

In 1919 Goddard thought that it would be premature to disclose the results of his experiments because his engine was not sufficiently developed. Webster realized that Goddard had accomplished a good deal of fine work and insisted that Goddard publish his progress so far or he would take care of it himself, so Goddard asked the Smithsonian Institution if it would publish the report, updated with notes, that he had submitted in late 1916.[16]: 102 

In late 1919, the Smithsonian published Goddard's groundbreaking work, A Method of Reaching Extreme Altitudes. The report describes Goddard's mathematical theories of rocket flight, his experiments with solid-fuel rockets, and the possibilities he saw of exploring Earth's atmosphere and beyond. Along with Konstantin Tsiolkovsky's earlier work, The Exploration of Cosmic Space by Means of Reaction Devices,[41] Goddard's report is regarded as one of the pioneering works of the science of rocketry, and 1750 copies were distributed worldwide.[42] Goddard also sent a copy to individuals who requested one, until his personal supply was exhausted. Smithsonian aerospace historian Frank Winter said that this paper was "one of the key catalysts behind the international rocket movement of the 1920s and 30s."[43]

Goddard described extensive experiments with solid-fuel rocket engines burning high-grade nitrocellulose smokeless powder. A critical breakthrough was the use of the steam turbine nozzle invented by the Swedish inventor Gustaf de Laval. The de Laval nozzle allows the most efficient (isentropic) conversion of the energy of hot gases into forward motion.[44] By means of this nozzle, Goddard increased the efficiency of his rocket engines from two percent to 64 percent and obtained supersonic exhaust velocities of over Mach 7.[22]: 44 [45]

Though most of this work dealt with the theoretical and experimental relations between propellant, rocket mass, thrust, and velocity, a final section, entitled "Calculation of minimum mass required to raise one pound to an 'infinite' altitude," discussed the possible uses of rockets, not only to reach the upper atmosphere but to escape from Earth's gravitation altogether.[46] He determined, using an approximate method to solve his differential equation of motion for vertical flight, that a rocket with an effective exhaust velocity (see specific impulse) of 7000 feet per second and an initial weight of 602 pounds would be able to send a one-pound payload to an infinite height. Included as a thought experiment was the idea of launching a rocket to the Moon and igniting a mass of flash powder on its surface, so as to be visible through a telescope. He discussed the matter seriously, down to an estimate of the amount of powder required. Goddard's conclusion was that a rocket with starting mass of 3.21 tons could produce a flash "just visible" from Earth, assuming a final payload weight of 10.7 pounds.[23]

Goddard eschewed publicity, because he did not have time to reply to criticism of his work, and his imaginative ideas about space travel were shared only with private groups he trusted. He did, though, publish and talk about the rocket principle and sounding rockets, since these subjects were not too "far out." In a letter to the Smithsonian, dated March 1920, he discussed: photographing the Moon and planets from rocket-powered fly-by probes, sending messages to distant civilizations on inscribed metal plates, the use of solar energy in space, and the idea of high-velocity ion propulsion. In that same letter, Goddard clearly describes the concept of the ablative heat shield, suggesting the landing apparatus be covered with "layers of a very infusible hard substance with layers of a poor heat conductor between" designed to erode in the same way as the surface of a meteor.[47]

Publicity and criticism

[edit]

Every vision is a joke until the first man accomplishes it; once realized, it becomes commonplace.

–Response to a reporter's question following criticism in The New York Times, 1920.[48][49]

The publication of Goddard's document gained him national attention from U.S. newspapers, most of it negative. Although Goddard's discussion of targeting the moon was only a small part of the work as a whole (eight lines on the next to last page of 69 pages), and was intended as an illustration of the possibilities rather than a declaration of intent, the papers sensationalized his ideas to the point of misrepresentation and ridicule. Even the Smithsonian had to abstain from publicity because of the amount of ridiculous correspondence received from the general public.[22]: 113  David Lasser, who co-founded the American Rocket Society (ARS), wrote in 1931 that Goddard was subjected in the press to the "most violent attacks."[50]

On January 12, 1920, a front-page story in The New York Times, "Believes Rocket Can Reach Moon", reported a Smithsonian press release about a "multiple-charge, high-efficiency rocket." The chief application envisaged was "the possibility of sending recording apparatus to moderate and extreme altitudes within the Earth's atmosphere", the advantage over balloon-carried instruments being ease of recovery, since "the new rocket apparatus would go straight up and come straight down." But it also mentioned a proposal "to [send] to the dark part of the new moon a sufficiently large amount of the most brilliant flash powder which, in being ignited on impact, would be plainly visible in a powerful telescope. This would be the only way of proving that the rocket had really left the attraction of the earth, as the apparatus would never come back, once it had escaped that attraction."[51]

New York Times editorial

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On January 13, 1920, the day after its front-page story about Goddard's rocket, an unsigned New York Times editorial, in a section entitled "Topics of the Times", scoffed at the proposal. The article, which bore the title "A Severe Strain on Credulity",[52] began with apparent approval, but soon went on to cast serious doubt:

As a method of sending a missile to the higher, and even highest, part of the earth's atmospheric envelope, Professor Goddard's multiple-charge rocket is a practicable, and therefore promising device. Such a rocket, too, might carry self-recording instruments, to be released at the limit of its flight, and conceivable parachutes would bring them safely to the ground. It is not obvious, however, that the instruments would return to the point of departure; indeed, it is obvious that they would not, for parachutes drift exactly as balloons do.[53]

The article pressed further on Goddard's proposal to launch rockets beyond the atmosphere:

[A]fter the rocket quits our air and really starts on its longer journey, its flight would be neither accelerated nor maintained by the explosion of the charges it then might have left. To claim that it would be is to deny a fundamental law of dynamics, and only Dr. Einstein and his chosen dozen, so few and fit, are licensed to do that. ... Of course, [Goddard] only seems to lack the knowledge ladled out daily in high schools.[54]

Thrust is however possible in a vacuum.[55]

Aftermath

[edit]

A week after the New York Times editorial, Goddard released a signed statement to the Associated Press, attempting to restore reason to what had become a sensational story:

Too much attention has been concentrated on the proposed flash pow[d]er experiment, and too little on the exploration of the atmosphere. ... Whatever interesting possibilities there may be of the method that has been proposed, other than the purpose for which it was intended, no one of them could be undertaken without first exploring the atmosphere.[56]

In 1924, Goddard published an article, "How my speed rocket can propel itself in vacuum", in Popular Science, in which he explained the physics and gave details of the vacuum experiments he had performed to prove the theory.[57] But, no matter how he tried to explain his results, he was not understood by the majority. After one of Goddard's experiments in 1929, a local Worcester newspaper carried the mocking headline "Moon rocket misses target by 238,79912 miles."[58]

Though the unimaginative public chuckled at the "moon man," his groundbreaking paper was read seriously by many rocketeers in America, Europe, and Russia who were stirred to build their own rockets. This work was his most important contribution to the quest to "aim for the stars."[59]: 50 

Goddard worked alone with just his team of mechanics and machinists for many years. This was a result of the harsh criticism from the media and other scientists, and his understanding of the military applications which foreign powers might use. Goddard became increasingly suspicious of others and often worked alone, except during the two World Wars, which limited the impact of much of his work. Another limiting factor was the lack of support from the American government, military and academia, all failing to understand the value of the rocket to study the atmosphere and near space, and for military applications.

Nevertheless, Goddard had some influence and was influenced by European rocketry pioneers like Hermann Oberth and his student Max Valier, at least as proponent of the idea of space rocketry and source of inspiration, although each side developed their technology and its scientific basis independently. In Europe the rocketeers were mainly theorists and visionaries. Goddard was the foremost experimenter, and his report was responsible for encouraging many to build their own rockets.

As Germany became ever more war-like, Goddard refused to communicate with German rocket experimenters, though he received more and more of their correspondence.[16]: 131  Oberth had Goddard's 1919 paper translated and Wernher von Braun read it. They therefore knew that efficiencies at least thirty times greater than conventional rockets were achievable with Goddard's engine design. Via von Braun and his team joining the US post-war programs there is thus an indirect line of scientific and technology tradition from NASA back to Goddard.

"A Correction"

[edit]

Forty-nine years after its editorial mocking Goddard, on July 17, 1969—the day after the launch of Apollo 11The New York Times published a short item under the headline "A Correction". The three-paragraph statement summarized its 1920 editorial and concluded:

Further investigation and experimentation have confirmed the findings of Isaac Newton in the 17th Century and it is now definitely established that a rocket can function in a vacuum as well as in an atmosphere. The Times regrets the error.[60]

First liquid-fueled flight

[edit]

Goddard began considering liquid propellants, including hydrogen and oxygen, as early as 1909. He knew that hydrogen and oxygen was the most efficient fuel/oxidizer combination. Liquid hydrogen was not readily available in 1921, however, and he selected gasoline as the safest fuel to handle.[23]: 13 

First static tests

[edit]
Robert Goddard, bundled against the cold weather of March 16, 1926, holds the launching frame of his most notable invention—the first liquid-fueled rocket.

Goddard began experimenting with liquid oxidizer, liquid fuel rockets in September 1921, and successfully tested the first liquid propellant engine in November 1923.[23]: 520  It had a cylindrical combustion chamber, using impinging jets to mix and atomize liquid oxygen and gasoline.[23]: 499–500 

In 1924–25, Goddard had problems developing a high-pressure piston pump to send fuel to the combustion chamber. He wanted to scale up the experiments, but his funding would not allow such growth. He decided to forgo the pumps and use a pressurized fuel feed system applying pressure to the fuel tank from a tank of inert gas, a technique that is still used today. The liquid oxygen, some of which evaporated, provided its own pressure.

On December 6, 1925, he tested the simpler pressure feed system. He conducted a static test on the firing stand at the Clark University physics laboratory. The engine successfully lifted its own weight in a 27-second test in the static rack. It was a major success for Goddard, proving that a liquid fuel rocket was possible.[16]: 140  The test moved Goddard an important step closer to launching a rocket with liquid fuel.

Goddard conducted an additional test in December, and two more in January 1926. After that, he began preparing for a possible launch of the rocket system.

First flight

[edit]

Goddard launched the world's first liquid-fueled (gasoline and liquid oxygen) rocket on March 16, 1926, in Auburn, Massachusetts. Present at the launch were his crew chief Henry Sachs, Esther Goddard, and Percy Roope, who was Clark's assistant professor in the physics department. Goddard's diary entry of the event was notable for its understatement:

March 16. Went to Auburn with S[achs] in am. E[sther] and Mr. Roope came out at 1 p.m. Tried rocket at 2.30. It rose 41 feet & went 184 feet, in 2.5 secs., after the lower half of the nozzle burned off. Brought materials to lab. ...[16]: 143 

His diary entry the next day elaborated:

March 17, 1926. The first flight with a rocket using liquid propellants was made yesterday at Aunt Effie's farm in Auburn. ... Even though the release was pulled, the rocket did not rise at first, but the flame came out, and there was a steady roar. After a number of seconds it rose, slowly until it cleared the frame, and then at express train speed, curving over to the left, and striking the ice and snow, still going at a rapid rate.[16]: 143 

The rocket, which was later dubbed "Nell", rose just 41 feet (12.5 meters) during a 2.5-second flight that ended 184 feet (56 meters) away in a cabbage field,[61] but it was an important demonstration that liquid fuels and oxidizers were possible propellants for larger rockets. The launch site is now a National Historic Landmark, the Goddard Rocket Launching Site.

Original launch console for launching Goddard liquid fuel rockets

Viewers familiar with more modern rocket designs may find it difficult to distinguish the rocket from its launching apparatus in the well-known picture of "Nell". The complete rocket is significantly taller than Goddard but does not include the pyramidal support structure which he is grasping. The rocket's combustion chamber is the small cylinder at the top; the nozzle is visible beneath it. The fuel tank, which is also part of the rocket, is the larger cylinder opposite Goddard's torso. The fuel tank is directly beneath the nozzle and is protected from the motor's exhaust by an asbestos cone. Asbestos-wrapped aluminum tubes connect the motor to the tanks, providing both support and fuel transport.[62] This layout is no longer used, since the experiment showed that this was no more stable than placing the combustion chamber and nozzle at the base. By May, after a series of modifications to simplify the plumbing, the combustion chamber and nozzle were placed in the now classic position, at the lower end of the rocket.[63]: 259 

Goddard determined early that fins alone were not sufficient to stabilize the rocket in flight and keep it on the desired trajectory in the face of winds aloft and other disturbing forces. He added movable vanes in the exhaust, controlled by a gyroscope, to control and steer his rocket. (The Germans used this technique in their V-2.) He also introduced the more efficient swiveling engine in several rockets, basically the method used to steer large liquid-propellant missiles and launchers today.[63]: 263–6 

Lindbergh and Goddard

[edit]

After launch of one of Goddard's rockets in July 1929 again gained the attention of the newspapers,[64] Charles Lindbergh learned of his work in a New York Times article. At the time, Lindbergh had begun to wonder what would become of aviation (even space flight) in the distant future and had settled on jet propulsion and rocket flight as a probable next step. After checking with the Massachusetts Institute of Technology (MIT) and being assured that Goddard was a bona fide physicist and not a crackpot, he phoned Goddard in November 1929.[22]: 141  Goddard met the aviator soon after in his office at Clark University.[65] Upon meeting Goddard, Lindbergh was immediately impressed by his research, and Goddard was similarly impressed by the flier's interest. He discussed his work openly with Lindbergh, forming an alliance that would last for the rest of his life. While having long since become reluctant to share his ideas, Goddard showed complete openness with those few who shared his dream, and whom he felt he could trust.[65]

By late 1929, Goddard had been attracting additional notoriety with each rocket launch. He was finding it increasingly difficult to conduct his research without unwanted distractions. Lindbergh discussed finding additional financing for Goddard's work and lent his famous name to Goddard's work. In 1930 Lindbergh made several proposals to industry and private investors for funding, which proved all but impossible to find following the recent U.S. stock market crash in October 1929.[65]

Guggenheim sponsorship

[edit]

In the spring of 1930, Lindbergh finally found an ally in the Guggenheim family. Financier Daniel Guggenheim agreed to fund Goddard's research over the next four years for a total of $100,000 (~$2.3 million today). The Guggenheim family, especially Harry Guggenheim, would continue to support Goddard's work in the years to come. The Goddards soon moved to Roswell, New Mexico[65]

Because of the military potential of the rocket, Goddard, Lindbergh, Harry Guggenheim, the Smithsonian Institution and others tried in 1940, before the U.S. entered World War II, to convince the Army and Navy of its value. Goddard's services were offered, but there was no interest, initially. Two young, imaginative military officers eventually got the services to attempt to contract with Goddard just prior to the war. The Navy beat the Army to the punch and secured his services to build variable-thrust, liquid-fueled rocket engines for jet-assisted take-off (JATO) of aircraft.[16]: 293–297  These rocket engines were the precursors to the larger throttlable rocket plane engines that helped launch the space age.[66]

Astronaut Buzz Aldrin wrote that his father, Edwin Aldrin Sr. "was an early supporter of Robert Goddard." The elder Aldrin was a student of physics under Goddard at Clark, and worked with Lindbergh to obtain the help of the Guggenheims. Buzz believed that if Goddard had received military support as Wernher von Braun's team had enjoyed in Germany, American rocket technology would have developed much more rapidly in World War II.[67]

Lack of vision in the United States

[edit]

Before World War II there was a lack of vision and serious interest in the United States concerning the potential of rocketry, especially in Washington. Although the Weather Bureau was interested beginning in 1929 in Goddard's rocket for atmospheric research, the Bureau could not secure governmental funding.[23]: 719, 746  Between the World Wars, the Guggenheim Foundation was the main source of funding for Goddard's research.[68]: 46, 59, 60  Goddard's liquid-fueled rocket was neglected by his country, according to aerospace historian Eugene Emme, but was noticed and advanced by other nations, especially the Germans.[42]: 63  Goddard showed remarkable prescience in 1923 in a letter to the Smithsonian. He knew that the Germans were very interested in rocketry and said he "would not be surprised if the research would become something in the nature of a race," and he wondered how soon the European "theorists" would begin to build rockets.[16]: 136  In 1936, the U.S. military attaché in Berlin asked Charles Lindbergh to visit Germany and learn what he could of their progress in aviation. Although the Luftwaffe showed him their factories and were open concerning their growing airpower, they were silent on the subject of rocketry. When Lindbergh told Goddard of this behavior, Goddard said, "Yes, they must have plans for the rocket. When will our own people in Washington listen to reason?"[16]: 272 

Most of the U.S.'s largest universities were also slow to realize rocketry's potential. Just before World War II, the head of the aeronautics department at MIT, at a meeting held by the Army Air Corps to discuss project funding, said that the California Institute of Technology (Caltech) "can take the Buck Rogers Job [rocket research]."[69] In 1941, Goddard tried to recruit an engineer for his team from MIT but could not find one who was interested.[16]: 326  There were some exceptions: MIT was at least teaching basic rocketry,[16]: 264  and Caltech had courses in rocketry and aerodynamics. After the war, Jerome Hunsaker of MIT, having studied Goddard's patents, stated that "Every liquid-fuel rocket that flies is a Goddard rocket."[16]: 363 

While away in Roswell, Goddard was still head of the physics department at Clark University, and Clark allowed him to devote most of his time to rocket research. Likewise, the University of California, Los Angeles (UCLA) permitted astronomer Samuel Herrick to pursue research in space vehicle guidance and control, and shortly after the war to teach courses in spacecraft guidance and orbit determination. Herrick began corresponding with Goddard in 1931 and asked if he should work in this new field, which he named astrodynamics. Herrick said that Goddard had the vision to advise and encourage him in his use of celestial mechanics "to anticipate the basic problem of space navigation." Herrick's work contributed substantially to America's readiness to control flight of Earth satellites and send men to the Moon and back.[70]

Roswell, New Mexico

[edit]
Charles Lindbergh took this picture of Robert H. Goddard's rocket, when he peered down the launching tower on September 23, 1935, in Roswell, New Mexico.
Goddard towing a rocket in Roswell

With new financial backing, Goddard eventually relocated to the Eden Valley Test Site in Roswell, New Mexico, in summer of 1930,[59]: 46  where he worked with his team of technicians in near-isolation and relative secrecy for years. He had consulted a meteorologist as to the best area to do his work, and Roswell seemed ideal. Here they would not endanger anyone, would not be bothered by the curious and would experience a more moderate climate (which was also better for Goddard's health).[16]: 177  The locals valued personal privacy, knew Goddard desired his, and when travelers asked where Goddard's facilities were located, they would likely be misdirected.[16]: 261 

By September 1931, his rockets had the now familiar appearance of a smooth casing with tail-fins. He began experimenting with gyroscopic guidance and made a flight test of such a system in April 1932. A gyroscope mounted on gimbals electrically controlled steering vanes in the exhaust, similar to the system used by the German V-2 over 10 years later. Though the rocket crashed after a short ascent, the guidance system had worked, and Goddard considered the test a success.[16]: 193–5 

A temporary loss of funding from the Guggenheims, as a result of the depression, forced Goddard in spring of 1932 to return to his much-loathed professorial responsibilities at Clark University.[71] He remained at the university until the autumn of 1934, when funding resumed.[72] Because of the death of the senior Daniel Guggenheim, the management of funding was taken on by his son, Harry Guggenheim.[72] Upon his return to Roswell, he began work on his A series of rockets, 4 to 4.5 meters long, and powered by gasoline and liquid oxygen pressurized with nitrogen. The gyroscopic control system was housed in the middle of the rocket, between the propellant tanks.[5]: xv, 15–46 

Gyroscope installed inside Goddard's 1939 series L-C rocket

The A-4 used a simpler pendulum system for guidance, as the gyroscopic system was being repaired. On March 8, 1935, it flew up to 1,000 feet, then turned into the wind and, Goddard reported, "roared in a powerful descent across the prairie, at close to, or at, the speed of sound." On March 28, 1935, the A-5 successfully flew vertically to an altitude of (0.91 mi; 4,800 ft) using his gyroscopic guidance system. It then turned to a nearly horizontal path, flew 13,000 feet and achieved a maximum speed of 550 miles per hour. Goddard was elated because the guidance system kept the rocket on a vertical path so well.[16]: 208 [23]: 978–9 

In 1936–1939, Goddard began work on the K and L series rockets, which were much more massive and designed to reach very high altitude. The K series consisted of static bench tests of a more powerful engine, achieving a thrust of 624 lbs in February 1936.[68] This work was plagued by trouble with chamber burn-through. In 1923, Goddard had built a regeneratively cooled engine, which circulated liquid oxygen around the outside of the combustion chamber, but he deemed the idea too complicated. He then used a curtain cooling method that involved spraying excess gasoline, which evaporated around the inside wall of the combustion chamber, but this scheme did not work well, and the larger rockets failed. Goddard returned to a smaller design, and his L-13 reached an altitude of 2.7 kilometers (1.7 mi; 8,900 ft), the highest of any of his rockets. Weight was reduced by using thin-walled fuel tanks wound with high-tensile-strength wire.[5]: 71–148 

Rocket weight reduction using thin-walled fuel tanks wound with high-tensile-strength wire
Top tank of L-C rocket

Goddard experimented with many of the features of today's large rockets, such as multiple combustion chambers and nozzles. In November 1936, he flew the world's first rocket (L-7) with multiple chambers, hoping to increase thrust without increasing the size of a single chamber. It had four combustion chambers, reached a height of 200 feet, and corrected its vertical path using blast vanes until one chamber burned through. This flight demonstrated that a rocket with multiple combustion chambers could fly stably and be easily guided.[5]: 96  In July 1937 he replaced the guidance vanes with a movable tail section containing a single combustion chamber, as if on gimbals (thrust vectoring). The flight was of low altitude, but a large disturbance, probably caused by a change in the wind velocity, was corrected back to vertical. In an August test the flight path was corrected seven times by the movable tail and was captured on film by Mrs Goddard.[5]: 113–116 

From 1940 to 1941, Goddard worked on the P series of rockets, which used propellant turbopumps (also powered by gasoline and liquid oxygen). The lightweight pumps produced higher propellant pressures, permitting a more powerful engine (greater thrust) and a lighter structure (lighter tanks and no pressurization tank), but two launches both ended in crashes after reaching an altitude of only a few hundred feet. The turbopumps worked well, however, and Goddard was pleased.[5]: 187–215 

When Goddard mentioned the need for turbopumps, Harry Guggenheim suggested that he contact pump manufacturers to aid him. None were interested, as the development cost of these miniature pumps was prohibitive. Goddard's team was therefore left on its own and from September 1938 to June 1940 designed and tested the small turbopumps and gas generators to operate the turbines. Esther later said that the pump tests were "the most trying and disheartening phase of the research."[16]: 274–5 

Goddard was able to flight-test many of his rockets, but many resulted in what the uninitiated would call failures, usually resulting from engine malfunction or loss of control. Goddard did not consider them failures, however, because he felt that he always learned something from a test.[59]: 45  Most of his work involved static tests, which are a standard procedure today, before a flight test. He wrote to a correspondent: "It is not a simple matter to differentiate unsuccessful from successful experiments. ... [Most] work that is finally successful is the result of a series of unsuccessful tests in which difficulties are gradually eliminated."[16]: 274 

General Jimmy Doolittle

[edit]

Jimmy Doolittle was introduced to the field of space science at an early point in its history. He recalls in his autobiography, "I became interested in rocket development in the 1930s when I met Robert H. Goddard, who laid the foundation. ... While with Shell Oil I worked with him on the development of a type of fuel. ... "[73] Harry Guggenheim and Charles Lindbergh arranged for (then Major) Doolittle to discuss with Goddard a special blend of gasoline. Doolittle flew himself to Roswell in October 1938 and was given a tour of Goddard's shop and a "short course" in rocketry. He then wrote a memo, including a rather detailed description of Goddard's rocket. In closing he said, "interplanetary transportation is probably a dream of the very distant future, but with the moon only a quarter of a million miles away—who knows!" In July 1941, he wrote Goddard that he was still interested in his rocket propulsion research. The Army was interested only in JATO at this point. However, Doolittle and Lindbergh were concerned about the state of rocketry in the US, and Doolittle remained in touch with Goddard.[23]: 1208–16, 1334, 1443 

Shortly after World War II, Doolittle spoke concerning Goddard to an American Rocket Society (ARS) conference at which a large number interested in rocketry attended. He later stated that at that time "we [in the aeronautics field] had not given much credence to the tremendous potential of rocketry."[74] In 1956, he was appointed chairman of the National Advisory Committee for Aeronautics (NACA) because the previous chairman, Jerome C. Hunsaker, thought Doolittle to be more sympathetic than other scientists and engineers to the rocket, which was increasing in importance as a scientific tool as well as a weapon.[73]: 516  Doolittle was instrumental in the successful transition of the NACA to the National Aeronautics and Space Administration (NASA) in 1958.[75] He was offered the position as first administrator of NASA, but he turned it down.[74]

Launch history

[edit]
Dr. Goddards original launch tower with blast deflector below rocket engine
Goddard blast deflector—view into side exhaust
Goddard blast deflector—side view of exhaust

Between 1926 and 1941, the following 35 rockets were launched:[3]

Date Type Altitude in feet Altitude in meters Flight duration Notes
March 16, 1926 Goddard 1 41 12.5 2.5 s first liquid rocket launch
April 3, 1926 Goddard 1 49 15 4.2 s record altitude
December 26, 1928 Goddard 3 16 5 unknown
July 17, 1929 Goddard 3 90 27 5.5 s record altitude
December 30, 1930 Goddard 4 2,000 610 unknown record altitude
September 29, 1931 Goddard 4 180 55 9.6 s
October 13, 1931 Goddard 4 1,700 520 unknown
October 27, 1931 Goddard 4 1,330 410 unknown
April 19, 1932 - 135 41 5 s
February 16, 1935 A series 650 200 unknown
March 8, 1935 A series 1,000 300 12 s
March 28, 1935 A series 4,800 1,460 20 s record altitude
May 31, 1935 A series 7,500 2,300 unknown record altitude
June 25, 1935 A series 120 37 10 s
July 12, 1935 A series 6,600 2,000 14 s
October 29, 1935 A series 4,000 1,220 12 s
July 31, 1936 L series, Section A 200 60 5 s
October 3, 1936 L-A 200 60 5 s
November 7, 1936 L-A 200 60 unknown 4 thrust chambers
December 18, 1936 L series, Section B 3 1 unknown Veered horizontally immediately after launch
February 1, 1937 L-B 1,870 570 20.5 s
February 27, 1937 L-B 1,500 460 20 s
March 26, 1937 L-B 8,000-9,000[4]: 340  2,500–2,700 22.3 s Highest altitude achieved
April 22, 1937 L-B 6,560 2,000 21.5 s
May 19, 1937 L-B 3,250 990 29.5 s
July 28, 1937 L-series, Section C 2,055 630 28 s Movable tail

steering

August 26, 1937 L-C 2,000 600 unknown Movable tail
November 24, 1937 L-C 100 30 unknown
March 6, 1938 L-C 525 160 unknown
March 17, 1938 L-C 2,170 660 15 s
April 20, 1938 L-C 4,215 1,260 25.3 s
May 26, 1938 L-C 140 40 unknown
August 9, 1938 L-C 4,920 (visual)
3,294 (barograph)
1,500
1,000
unknown
August 9, 1940 P-series, Section C 300 90 unknown
May 8, 1941 P-C 250 80 unknown
Goddard L-C rocket
Top view of 1939 L-C series rocket.
Some of the parts of Goddard's rockets

Analysis of results

[edit]

As an instrument for reaching extreme altitudes, Goddard's rockets were not very successful; they did not achieve an altitude greater than 2.7 km in 1937, while a balloon sonde had already reached 35 km in 1921.[23]: 456  By contrast, German rocket scientists had achieved an altitude of 2.4 km with the A-2 rocket in 1934,[33]: 138  8 km by 1939 with the A-5,[76]: 39  and 176 km in 1942 with the A-4 (V-2) launched vertically, reaching the outer limits of the atmosphere and into space.[77]: 221 

Goddard's pace was slower than the Germans' because he did not have the resources they did. Simply reaching high altitudes was not his primary goal; he was trying, with a methodical approach, to perfect his liquid fuel engine and subsystems such as guidance and control so that his rocket could eventually achieve high altitudes without tumbling in the rare atmosphere, providing a stable vehicle for the experiments it would eventually carry. He had built the necessary turbopumps and was on the verge of building larger, lighter, more reliable rockets to reach extreme altitudes carrying scientific instruments when World War II intervened and changed the path of American history. He hoped to return to his experiments in Roswell after the war.[16]: 206, 230, 330–1 [23]: 923–4 

Though by the end of the Roswell years much of his technology had been replicated independently by others, he introduced new developments to rocketry that were used in this new enterprise: lightweight turbopumps, variable-thrust engine (in U.S.), engine with multiple combustion chambers and nozzles, and curtain cooling of combustion chamber.

Although Goddard had brought his work in rocketry to the attention of the United States Army, between World Wars, he was rebuffed, since the Army largely failed to grasp the military application of large rockets and said there was no money for new experimental weapons.[16]: 297  German military intelligence, by contrast, had paid attention to Goddard's work. The Goddards noticed that some mail had been opened, and some mailed reports had gone missing. An accredited military attaché to the US, Friedrich von Boetticher, sent a four-page report to the Abwehr in 1936, and the spy Gustav Guellich sent a mixture of facts and made-up information, claiming to have visited Roswell and witnessed a launch. The Abwehr was very interested and responded with more questions about Goddard's work.[78]: 77 [22]: 227–8  Guellich's reports did include information about fuel mixtures and the important concept of fuel-curtain cooling,[79]: 39–41  but thereafter the Germans received very little information about Goddard.

The Soviet Union had a spy (name still not declassified as of 2009) in the U.S. Navy Bureau of Aeronautics. In 1935, she gave them a report Goddard had written for the Navy in 1933. It contained results of tests and flights and suggestions for military uses of his rockets. The Soviets considered this to be very valuable information. It provided few design details, but gave them the direction and knowledge about Goddard's progress.[80]: 386–7 

Annapolis, Maryland

[edit]

Navy Lieutenant Charles F. Fischer, who had visited Goddard in Roswell earlier and gained his confidence, believed Goddard was doing valuable work and was able to convince the Bureau of Aeronautics in September 1941 that Goddard could build the JATO unit the Navy desired. While still in Roswell, and before the Navy contract took effect, Goddard began in September to apply his technology to build a variable-thrust engine to be attached to a PBY seaplane. By May 1942, he had a unit that could meet the Navy's requirements and be able to launch a heavily loaded aircraft from a short runway. In February, he received part of a PBY with bullet holes apparently acquired in the Pearl Harbor attack. Goddard wrote to Guggenheim that "I can think of nothing that would give me greater satisfaction than to have it contribute to the inevitable retaliation."[16]: 322, 328–9, 331, 335, 337 

In April, Fischer notified Goddard that the Navy wanted to do all its rocket work at the Engineering Experiment Station at Annapolis. Esther, worried that a move to the climate of Maryland would cause Robert's health to deteriorate faster, objected. But the patriotic Goddard replied, "Esther, don't you know there's a war on?" Fischer also questioned the move, as Goddard could work just as well in Roswell. Goddard simply answered, "I was wondering when you would ask me." Fischer had wanted to offer him something bigger—a long range missile—but JATO was all he could manage, hoping for a greater project later.[16]: 338, 9  It was a case of a square peg in a round hole, according to a disappointed Goddard.[22]: 209 

Goddard and his team had already been in Annapolis a month and had tested his constant-thrust JATO engine when he received a Navy telegram, forwarded from Roswell, ordering him to Annapolis. Lt. Fischer asked for a crash effort. By August, his engine was producing 800 lbs of thrust for 20 seconds, and Fischer was anxious to try it on a PBY. On the sixth test run, with all bugs worked out, the PBY, piloted by Fischer, was pushed into the air from the Severn River. Fischer landed and prepared to launch again. Goddard had wanted to check the unit, but radio contact with the PBY had been lost. On the seventh try, the engine caught fire. The plane was 150 feet up when flight was aborted. Because Goddard had installed a safety feature at the last minute, there was no explosion and there were no deaths. The problem's cause was traced to hasty installation and rough handling. Cheaper, safer solid fuel JATO engines were eventually selected by the armed forces. An engineer later said, "Putting [Goddard's] rocket on a seaplane was like hitching an eagle to a plow."[16]: 344–50 

Goddard's first biographer Milton Lehman notes:

In its 1942 crash effort to perfect an aircraft booster, the Navy was beginning to learn its way in rocketry. In similar efforts, the Army Air Corps was also exploring the field [with GALCIT]. Compared to Germany's massive program, these beginnings were small, yet essential to later progress. They helped develop a nucleus of trained American rocket engineers, the first of the new breed who would follow the professor into the Age of Space.[16]: 350 

In August 1943, President Atwood at Clark wrote to Goddard that the university was losing the acting head of the physics department, was taking on "emergency work" for the army, and he was to "report for duty or declare the position vacant." Goddard replied that he believed he was needed by the navy, was nearing retirement age, and was unable to lecture because of his throat problem, which did not allow him to talk above a whisper. He regretfully resigned as professor of physics and expressed his deepest appreciation for all Atwood and the trustees had done for him and indirectly for the war effort.[23]: 1509–11  In June he had gone to see a throat specialist in Baltimore, who recommended that he not talk at all, to give his throat a rest.[23]: 1503 

The station, under Lt Commander Robert Truax, was developing another JATO engine in 1942 that used hypergolic propellants, eliminating the need for an ignition system. Chemist Ensign Ray Stiff had discovered in the literature in February that aniline and nitric acid burned fiercely immediately when mixed.[23]: 1488 [33]: 172  Goddard's team built the pumps for the aniline fuel and the nitric acid oxidizer and participated in the static testing.[23]: 1520, 1531  The Navy delivered the pumps to Reaction Motors (RMI) to use in developing a gas generator for the pump turbines. Goddard went to RMI to observe testing of the pump system and would eat lunch with the RMI engineers.[23]: 1583  (RMI was the first firm formed to build rocket engines and built engines for the Bell X-1 rocket plane[10]: 1  and Viking (rocket).[10]: 169  RMI offered Goddard one-fifth interest in the company and a partnership after the war.[23]: 1583 ) Goddard went with Navy people in December 1944 to confer with RMI on division of labor, and his team was to provide the propellant pump system for a rocket-powered interceptor because they had more experience with pumps.[10]: 100  He consulted with RMI from 1942 through 1945.[63]: 311  Though previously competitors, Goddard had a good working relationship with RMI, according to historian Frank H. Winter.[81]

The Navy had Goddard build a pump system for Caltech's use with acid-aniline propellants. The team built a 3000-lb thrust engine using a cluster of four 750-lb thrust motors.[23]: 1574, 1592  They also developed 750-lb engines for the Navy's Gorgon guided interceptor missile (experimental Project Gorgon). Goddard continued to develop the variable-thrust engine with gasoline and lox because of the hazards involved with the hypergolics.[23]: 1592 [16]: 355, 371 

Despite Goddard's efforts to convince the Navy that liquid-fueled rockets had greater potential, he said that the Navy had no interest in long-range missiles.[23]: 1554  However, the Navy asked him to perfect the throttleable JATO engine. Goddard made improvements to the engine, and in November it was demonstrated to the Navy and some officials from Washington. Fischer invited the spectators to operate the controls; the engine blasted out over the Severn at full throttle with no hesitation, idled, and roared again at various thrust levels. The test was perfect, exceeding the Navy's requirements. The unit was able to be stopped and restarted, and it produced a medium thrust of 600 pounds for 15 seconds and a full thrust of 1,000 pounds for over 15 seconds. A Navy Commander commented that "It was like being Thor, playing with thunderbolts." Goddard had produced the essential propulsion control system of the rocket plane. The Goddards celebrated by attending the Army-Navy football game and attending the Fischers' cocktail party.[23]: 350–1 

This engine was the basis of the Curtiss-Wright XLR25-CW-1 two-chamber, 15,000-pound variable-thrust engine that powered the Bell X-2 research rocket plane. After World War II, Goddard's team and some patents went to Curtiss-Wright Corporation. "Although his death in August 1945 prevented him from participating in the actual development of this engine, it was a direct descendent of his design."[23]: 1606  Clark University and the Guggenheim Foundation received the royalties from the use of the patents.[82] In September 1956, the X-2 was the first plane to reach 126,000 feet altitude and in its last flight exceeded Mach 3 (3.2) before losing control and crashing. The X-2 program advanced technology in areas such as steel alloys and aerodynamics at high Mach numbers.[83]

The German V-2

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Don't you know about your own rocket pioneer? Dr. Goddard was ahead of us all.

Wernher von Braun, when asked about his work, following World War II[43]

In the spring of 1945, Goddard saw a captured German V-2 ballistic missile, in the naval laboratory in Annapolis, Maryland, where he had been working under contract. The unlaunched rocket had been captured by the US Army from the Mittelwerk factory in the Harz mountains in Germany and samples began to be shipped by Special Mission V-2 on 22 May 1945.[76]

After a thorough inspection, Goddard was convinced that the Germans had "stolen" his work. Though the design details were not exactly the same, the basic design of the V-2 was similar to one of Goddard's rockets. The V-2, however, was technically far more advanced than the most successful of the rockets designed and tested by Goddard. The Peenemünde rocket group led by Wernher von Braun may have benefited from the pre-1939 contacts to a limited extent,[16]: 387–8  but had also started from the work of their own space pioneer, Hermann Oberth; they also had the benefit of intensive state funding, large-scale production facilities (using slave labor), and repeated flight-testing that allowed them to refine their designs. Oberth was a space flight theorist and had never built a rocket, but he tested small liquid propellant thrust chambers in 1929–30 which were not advances in the "state of the art".[63]: 273, 275  In 1922 Oberth asked Goddard for a copy of his 1919 paper and was sent one though Goddard was distrustful of the militaristic Germans.[22]: 96  Later, Oberth erroneously believed that Goddard lacked vision, was interested only in studying the atmosphere, and did not comprehend the future of rocketry for space exploration.

Nevertheless, in 1963, von Braun, reflecting on the history of rocketry, said of Goddard: "His rockets ... may have been rather crude by present-day standards, but they blazed the trail and incorporated many features used in our most modern rockets and space vehicles".[84] He once recalled that "Goddard's experiments in liquid fuel saved us years of work, and enabled us to perfect the V-2 years before it would have been possible."[85] After World War II von Braun reviewed Goddard's patents and believed they contained enough technical information to build a large missile.[86]

Three features developed by Goddard appeared in the V-2: (1) turbopumps were used to inject fuel into the combustion chamber; (2) gyroscopically controlled vanes in the nozzle exhaust stabilized the rocket until external vanes in the air could do so; and (3) excess alcohol was fed in around the combustion chamber walls, so that a blanket of evaporating gas protected the engine walls from the combustion heat. [87]

The Germans had been watching Goddard's progress before the war and became convinced that large, liquid fuel rockets were feasible. General Walter Dornberger, head of the V-2 project, used the idea that they were in a race with the U.S. and that Goddard had "disappeared" (to work with the Navy) as a way to persuade Hitler to raise the priority of the V-2.

Goddard's secrecy

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Goddard avoided sharing details of his work with other scientists and preferred to work alone with his technicians.[88] Frank Malina, who was then studying rocketry at the California Institute of Technology, visited Goddard in August 1936. Goddard hesitated to discuss any of his research, other than that which had already been published in Liquid-Propellant Rocket Development. Theodore von Kármán, Malina's mentor at the time, was unhappy with Goddard's attitude and later wrote, "Naturally we at Caltech wanted as much information as we could get from Goddard for our mutual benefit. But Goddard believed in secrecy. ... The trouble with secrecy is that one can easily go in the wrong direction and never know it."[89]: 90  However, at an earlier point, von Kármán said that Malina was "highly enthusiastic" after his visit and that Caltech made changes to their liquid-propellant rocket, based on Goddard's work and patents. Malina remembered his visit as friendly and that he saw all but a few components in Goddard's shop.[22]: 178 

Goddard's concerns about secrecy led to criticism for failure to cooperate with other scientists and engineers. His approach at that time was that independent development of his ideas without interference would bring quicker results even though he received less technical support. George Sutton, who became a rocket scientist working with von Braun's team in the late 1940s, said that he and his fellow workers had not heard of Goddard or his contributions and that they would have saved time if they had known the details of his work. Sutton admits that it may have been their fault for not looking for Goddard's patents and depending on the German team for knowledge and guidance; he wrote that information about the patents was not well distributed in the U.S. at that early period after World War II, though Germany and the Soviet Union had copies of some of them. (The Patent Office did not release rocket patents during World War II.)[63] However, the Aerojet Engineering Corporation, an offshoot of the Guggenheim Aeronautical Laboratory at Caltech (GALCIT), filed two patent applications in Sep 1943 referencing Goddard's U.S. patent 1,102,653 for the multistage rocket.

By 1939, von Kármán's GALCIT had received Army Air Corps funding to develop rockets to assist in aircraft take-off. Goddard learned of this in 1940, and openly expressed his displeasure at not being considered.[89] Malina could not understand why the Army did not arrange for an exchange of information between Goddard and Caltech since both were under government contract at the same time. Goddard did not think he could be of that much help to Caltech because they were designing rocket engines mainly with solid fuel, while he was using liquid fuel.

Goddard was concerned with avoiding the public criticism and ridicule he had faced in the 1920s, which he believed had harmed his professional reputation. He also lacked interest in discussions with people who had less understanding of rocketry than he did,[16]: 171  feeling that his time was extremely constrained.[16]: 23  Goddard's health was frequently poor, as a result of his earlier bout of tuberculosis, and he was uncertain about how long he had to live.[16]: 65, 190  He felt, therefore, that he hadn't the time to spare arguing with other scientists and the press about his new field of research, or helping all the amateur rocketeers who wrote to him.[16]: 61, 71, 110–11, 114–15  In 1932 Goddard wrote to H. G. Wells:

How many more years I shall be able to work on the problem, I do not know; I hope, as long as I live. There can be no thought of finishing, for "aiming at the stars", both literally and figuratively, is a problem to occupy generations, so that no matter how much progress one makes, there is always the thrill of just beginning.[20]

Goddard spoke to professional groups, published articles and papers and patented his ideas; but while he discussed basic principles, he was unwilling to reveal the details of his designs until he had flown rockets to high altitudes and thus proven his theory.[16]: 115  He tended to avoid any mention of space flight, and spoke only of high-altitude research, since he believed that other scientists regarded the subject as unscientific.[16]: 116  GALCIT saw Goddard's publicity problems and that the word "rocket" was "of such bad repute" that they used the word "jet" in the name of JPL and the related Aerojet Engineering Corporation.[90]

Many authors writing about Goddard mention his secrecy, but neglect the reasons for it. Some reasons have been noted above. Much of his work was for the military and was classified.[23]: 1541  There were some in the U.S. before World War II that called for long-range rockets, and in 1939 Major James Randolph wrote a "provocative article" advocating a 3000-mile range missile. Goddard was "annoyed" by the unclassified paper as he thought the subject of weapons should be "discussed in strict secrecy."[91]

However, Goddard's tendency to secrecy was not absolute, nor was he totally uncooperative. In 1945 GALCIT was building the WAC Corporal for the Army. But they were having trouble with their liquid propellant rocket engine's performance (timely, smooth ignition and explosions). Frank Malina went to Annapolis in February and consulted with Goddard and Stiff, and they arrived at a solution to the problem (hypergolic propellant: nitric acid and aniline), which resulted in the successful launch of the high-altitude research rocket in October 1945.[92]

During the First and Second World Wars, Goddard offered his services, patents, and technology to the military, and made some significant contributions. Just before the Second World War several young Army officers and a few higher-ranking ones believed Goddard's research was important but were unable to generate funds for his work.[93]

Toward the end of his life, Goddard, realizing he was no longer going to be able to make significant progress alone in his field, joined the American Rocket Society and became a director. He made plans to work in the budding US aerospace industry (with Curtiss-Wright), taking most of his team with him.[16]: 382, 385 

Personal life

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On June 21, 1924, Goddard married Esther Christine Kisk (March 31, 1901 – June 4, 1982),[94] a secretary in Clark University's President's office, whom he had met in 1919. She became enthusiastic about rocketry and photographed some of his work as well as aided him in his experiments and paperwork, including accounting. They enjoyed going to the movies in Roswell and participated in community organizations such as the Rotary and the Woman's Club. He painted the New Mexican scenery, sometimes with the artist Peter Hurd, and played the piano. She played bridge, while he read. Esther said Robert participated in the community and readily accepted invitations to speak to church and service groups. The couple did not have children. After his death, she sorted out Goddard's papers, and secured 131 additional patents on his work.[95]

Concerning Goddard's religious views, he was raised as an Episcopalian, though he was not outwardly religious.[96] The Goddards were associated with the Episcopal church in Roswell, and he attended occasionally. He once spoke to a young people's group on the relationship of science and religion.[16]: 224 

Goddard's serious bout with tuberculosis weakened his lungs, affecting his ability to work, and was one reason he liked to work alone, in order to avoid argument and confrontation with others and use his time fruitfully. He labored with the prospect of a shorter than average life span.[16]: 190  After arriving in Roswell, Goddard applied for life insurance, but when the company doctor examined him he said that Goddard belonged in a bed in Switzerland (where he could get the best care).[16]: 183  Goddard's health began to deteriorate further after moving to the humid climate of Maryland to work for the Navy. He was diagnosed with throat cancer in 1945. He continued to work, able to speak only in a whisper until surgery was required, and he died in August of that year in Baltimore, Maryland.[16]: 377, 395 [97] He was buried in Hope Cemetery in his home town of Worcester, Massachusetts.[98]

Legacy

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Influence

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Obelisk marks the Goddard Rocket Launching Site
  • The Goddard Rocket Launching Site in Auburn, Massachusetts, is a National Historic Landmark. The location was formerly the Asa Ward Farm, and is now a golf course.[105]
  • New Goddard prototype experimental reusable vertical launch and landing rocket from Blue Origin is named after Goddard.[106]
  • The Dr. Robert H. Goddard Award, also known as the Achievement 7 Award, is an award given to cadets of the Civil Air Patrol who reach the rank of Cadet Chief Master Sergeant. The promotion and the award are always given concurrently and in unison with one another.[107]
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  • Children's author Isabel Hornibrook, in her novel Pemrose Lorry: Campfire Girl (Little, Brown and Company, 1921) claimed in the preface to have been the first to exploit Goddard's rocket as a plot device. In the last chapter, she wrote, "And never–oh! never since the history of Mother Earth and her satellite began did such a spectacular traveler start on such a flaming trip as when the hand of a Camp Fire Girl of America threw the switch and the steel explorer, twenty feet long, leaped from its platform high into the air, pointed directly for the moon, with a great inventor's mathematical precision,–trailing its two-hundred-foot, rosy trail of fire. There was not breath–not breath, even, to cry: "Watch it tear!"[108]
  • In F.L.A.S.H.!, episode 10 of season 11 of the Canadian television period drama Murdoch Mysteries (January 8, 2018), Goddard is played by Andrew Robinson and is described as a rocket scientist and chief scientist for a fictional pneumatic tube public transport system in early 1900s Toronto, Canada.[109]
  • Rocket, an American pale ale made by the Wormtown Brewery of Worcester, Massachusetts is named in Goddard's honor.[110]

Patents of interest

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Goddard received 214 patents for his work, of which 131 were awarded after his death.[99] Among the most influential patents were:

The Guggenheim Foundation and Goddard's estate filed suit in 1951 against the U.S. government for prior infringement of three of Goddard's patents.[99] In 1960, the parties settled the suit, and the U.S. armed forces and NASA paid out an award of $1 million: half of the award settlement went to his wife, Esther. At that time, it was the largest government settlement ever paid in a patent case.[99][16]: 404  The settlement amount exceeded the total amount of all the funding that Goddard received for his work, throughout his entire career.

Important firsts

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  • First American to explore mathematically the practicality of using rocket propulsion to reach high altitudes and to traject to the Moon (1912)[111]
  • First to receive a U.S. patent on the idea of a multistage rocket (1914)[111]
  • First to static test a rocket in a systematic, scientific manner, measuring thrust, exhaust velocity and efficiency. He obtained the highest efficiency of any heat engine at the time. (1915-1916)[111]: 7 [16]: 78 
  • First to prove that rocket propulsion operates in a vacuum (which was doubted by some scientists of that time), that it needs no air to push against. He actually obtained a 20% increase in efficiency over that determined at ground-level atmospheric pressure (1915–1916).[111]: 7 [16]: 76 
  • First to prove that an oxidizer and a fuel could be mixed using injectors and burned controllably in a combustion chamber, also doubted by physicists.[63]: 256 
  • First to develop suitable lightweight centrifugal pumps for liquid-fuel rockets and also gas generators to drive the pump turbine (1923).[111][63]: 260 
  • First to attach a DeLaval type of nozzle to the combustion chamber of a solid-fuel engine and increase efficiency by more than ten times. The exhaust flow became supersonic at the narrowest cross-sectional area (throat) of the nozzle.[63]: 257 
  • First to develop the liquid propellant feed system using a high-pressure gas to force the propellants from their tanks into the thrust chamber (1923).[63]: 257 
  • First to develop and successfully fly a liquid-propellant rocket (March 16, 1926)[111]
  • First to launch a scientific payload (a barometer, a thermometer, and a camera) in a rocket flight (1929)[111]
  • First to use vanes in the rocket engine exhaust for guidance (1932)[111]
  • First to develop gyroscopic control apparatus for guiding rocket flight (1932)[111]
  • First to launch and successfully guide a rocket with an engine pivoted by moving the tail section (as if on gimbals) controlled by a gyro mechanism (1937)[111]
  • Built lightweight propellant tanks out of thin sheets of steel and aluminum and used external high-strength steel wiring for reinforcement. He introduced baffles in the tanks to minimize sloshing which changed the center gravity of the vehicle. He used insulation on the very cold liquid-oxygen components.[63]: 258, 259 
  • First in U.S. to design and test a variable-thrust rocket engine.[63]: 266 
  • First to fly a rocket with an engine having multiple (four) thrust chambers.[63]: 266 
  • First to test regenerative cooling of the thrust chamber in March 1923 (first suggested by Tsiolkovsky but unknown to Goddard).[10]

Bibliography

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See also

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References

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Revisions and contributorsEdit on WikipediaRead on Wikipedia
from Grokipedia
Robert Hutchings Goddard (October 5, 1882 – August 10, 1945) was an American , , and inventor regarded as the father of modern rocketry for his pioneering development of technology. Born in , Goddard conducted foundational experiments in rocketry beginning in the early , driven by theoretical insights into and high-altitude flight. In 1914, he secured U.S. patents for a liquid-fueled and a multi-stage design, concepts that anticipated key elements of future vehicles. Goddard's most notable achievement came on March 16, 1926, when he launched the world's first from a farm in , using and as propellants, reaching a height of 41 feet. Over his career, he amassed 214 patents related to components and systems, many of which formed the basis for advancements in missiles and during and after . Though his work encountered funding shortages and public skepticism, including ridicule from the press, Goddard's empirical demonstrations and innovations established causal principles of efficient rocketry that propelled subsequent engineering progress.

Early Life and Influences

Childhood Experiments and Mechanical Aptitude

Robert H. Goddard, born on October 5, 1882, in , exhibited early mechanical aptitude through hands-on experimentation despite frequent childhood illnesses that caused prolonged absences from school and necessitated . These health setbacks, including bouts of and , afforded him ample time for self-directed projects, fostering a systematic approach to invention and documentation of his trials. From boyhood, Goddard displayed a unique genius for mechanical construction, beginning with simple devices involving flight mechanisms such as kites and balloons, which honed his skills in materials shaping and assembly. One notable early project involved attempting to build a hot air balloon using sheets of aluminum foil, an endeavor that demonstrated his resourcefulness in sourcing and manipulating lightweight materials, though it ultimately failed to achieve lift. By age 16, around 1898 during his high school years at Worcester South High School, Goddard's interests converged on more ambitious constructs; he shaped raw aluminum into a balloon envelope in his home workshop and filled it with hydrogen, aiming for ascension to carry weather instruments aloft, but the design proved insufficient for flight. These efforts reflected an innate aptitude for prototyping, as he meticulously tested material properties and propulsion concepts, laying groundwork for later propulsion studies. In high school, Goddard extended his mechanical pursuits to chemical experimentation, attempting to compress graphite using hydrogen gas to explore potential applications in propulsion or materials science, further evidencing his precocious engineering mindset. Such boyhood activities, conducted amid limited formal resources, underscored his persistence and empirical method, prioritizing iterative testing over theoretical abstraction alone. This phase of self-taught mechanical proficiency not only built practical skills but also ignited a lifelong commitment to solving aerial and propulsion challenges through tangible fabrication.

Inspirational Dream and Literary Sparks

On October 19, 1899, at the age of 17, Goddard experienced a pivotal moment of inspiration while climbing a cherry in his family's backyard in . Gazing at the sky, he envisioned a mechanical device capable of propelling humans to Mars and beyond, an idea he recorded in his diary as the genesis of his lifelong pursuit of rocketry. This "cherry tree vision," as it became known, marked a shift from general scientific curiosity to a focused dream of , though Goddard later reflected on it as a youthful fancy tempered by rigorous engineering. Goddard's aspirations were sparked earlier by science fiction literature, particularly H.G. Wells' The War of the Worlds, which he read at age 16 shortly after its 1898 publication. The novel's depiction of Martian cylinders arriving on Earth via advanced propulsion ignited his imagination about spaceflight, prompting him to consider rockets as a feasible means to overcome gravity. Wells' influence persisted; Goddard corresponded with him decades later, affirming in a 1932 letter that the author's works had fueled his conviction in the practicality of aiming "at the stars, both literally and figuratively." While other writers like Jules Verne contributed to the era's speculative fiction, Wells' narrative of interplanetary invasion provided the most direct literary catalyst for Goddard's technical ambitions.

Formal Education and Initial Academic Pursuits

Goddard completed his secondary education at South High School in , graduating in 1904. He then enrolled at (WPI), where he majored in general science and received a degree in 1908. After graduation, he remained at WPI as an instructor in the physics department for two years, during which time he conducted early experiments with powder rockets in the institution's basement in 1907. In 1909, Goddard began graduate studies at in Worcester, initially enrolling as a special student in physics before advancing to a fellowship. He earned a degree in physics in 1910, with a on the theory of , and completed his in physics the following year. His doctoral research focused on problems related to charged particles and high-vacuum apparatus, which later informed his rocketry investigations. Following his Ph.D., Goddard accepted a position as an instructor in physics at , where he taught and conducted research for over two decades. In this early academic role, he presented theoretical work on novel methods for attaining high altitudes, marking the inception of his systematic pursuit of rocket principles.

Theoretical and Patent Innovations

Derivation of Rocket Propulsion Mathematics

In his 1919 Smithsonian publication A Method of Reaching Extreme Altitudes, Robert H. Goddard outlined the core of rocket propulsion by applying conservation of momentum to the expulsion of mass in a , independent of atmospheric resistance or gravity for the foundational case. He modeled an "ideal " where is ejected rearward at a constant cc, with initial total mass MM decreasing as mass mm (positive quantity) is expelled over time tt, leaving instantaneous mass MmM - m. To account for structural mass, Goddard introduced kk as the inert fraction of ejected material (casing or non-propellant), yielding an effective ejection velocity c(1k)c(1 - k). The derivation begins with the momentum balance: the forward impulse on the rocket equals the backward momentum of the exhaust. For infinitesimal expulsion dm>0dm > 0, the rocket's velocity increase dvdv satisfies (Mm)dv=c(1k)dm(M - m) \, dv = c(1 - k) \, dm, as the remaining mass gains momentum while the expelled dmdm carries away momentum at relative speed c(1k)c(1 - k). Rearranging gives the differential equation dv=c(1k)Mmdmdv = \frac{c(1 - k)}{M - m} \, dm. Integrating from initial velocity v=0v = 0 at m=0m = 0 to final velocity vv at total ejected mass mm, with boundaries mm from 0 to mm and vv from 0 to vv, yields v=c(1k)ln(MMm)v = c(1 - k) \ln \left( \frac{M}{M - m} \right). For the pure propellant idealization (k=0k = 0), this simplifies to v=cln(MMf)v = c \ln \left( \frac{M}{M_f} \right), where Mf=MmM_f = M - m is the final payload mass, demonstrating logarithmic velocity gain proportional to the mass ratio and independent of expulsion rate. This equation quantifies the thrust mechanism: acceleration arises solely from internal reaction, enabling propulsion in vacuum, contrary to contemporary skepticism rooted in misconceptions of Newton's third law requiring an external medium. Goddard extended the model to vertical ascent by incorporating gravity, deriving a more complex dvdt=g+c(1k)Mmdmdt\frac{dv}{dt} = -g + \frac{c(1 - k)}{M - m} \frac{dm}{dt}, solved approximately via stepwise intervals for altitude HH and required initial mass. For instance, achieving parabolic (approximately 6.95 miles per second) to reach from Earth's surface demanded an initial such that M602M \approx 602 pounds per 1 pound , assuming c(1k)=7,000c(1 - k) = 7,000 ft/s and a=150a = 150 ft/s². These derivations, first conceptualized by around 1912, provided the analytical foundation for multi-stage designs and liquid propellants to maximize cc and minimize kk.

Foundational Patents for Liquid and Multi-Stage Rockets

In 1914, Robert H. Goddard secured two pivotal U.S. patents that laid the groundwork for modern by addressing key limitations of solid-fuel designs prevalent at the time. U.S. Patent No. 1,102,653, issued on July 7, 1914, described a multi-stage apparatus capable of achieving higher altitudes through sequential ignition and jettisoning of spent stages, thereby reducing and increasing as the rocket ascended. This innovation stemmed from Goddard's calculations on the rocket equation, recognizing that staging minimized the inertial burden of exhausted , though the patent initially focused on solid propellants for practical ignition sequencing. One week later, on July 14, 1914, Goddard received U.S. No. 1,103,503 for a liquid-fueled rocket apparatus, which introduced controllable via liquid propellants—specifically as fuel and or as oxidizer—pumped into a for sustained . Unlike solid fuels, which burned uncontrollably once ignited, this design allowed for throttling and reignition potential, addressing Goddard's empirical observations of solid propellants' inefficiencies in achieving precise, high-altitude trajectories. The detailed a feed system using pressurized gases to force liquids into the , foreshadowing later pump-fed engines, though early implementations relied on simple pressure differentials due to technological constraints. These patents, filed in May 1914 amid Goddard's theoretical work at , represented first-principles advancements: multi-staging optimized payload-to-velocity ratios per the Tsiolkovsky equation Goddard had derived independently, while liquid propulsion enabled higher specific impulses through denser and combustion control. Though not immediately prototyped at scale—Goddard's first liquid-fueled flight occurred in —they established that influenced subsequent rocketry, with Goddard holding over 200 patents by his death, many building on these foundations. Skepticism from contemporaries, who viewed liquid handling as impractical, delayed adoption, but the designs' causal logic—prioritizing efficiency over simplicity—proved prescient in enabling .

Health Setbacks Amid Persistent Development

In early 1913, Goddard was diagnosed with advanced , the same illness that had afflicted his mother, with physicians initially estimating he had only weeks to live. Refused admission to a sanitarium due to his critical condition, he recuperated at home under medical care, gradually regaining enough strength to resume intellectual pursuits despite persistent frailty. This health crisis interrupted his brief research fellowship at , which he had begun in 1912, forcing his return to . Despite the setback, Goddard's focus on rocketry theory intensified during recovery, culminating in the filing of patent applications in May 1913 for a design and related apparatus. These efforts persisted amid ongoing physical limitations, leading to the U.S. granting his first two rocketry patents on July 7, 1914—one for a system and another for a apparatus using —fundamental innovations that addressed inefficiencies in solid-fuel . By 1915, while still convalescing, he conducted initial static tests of solid-fuel rockets at , demonstrating his determination to advance experimental validation of his mathematical derivations on in conditions. Goddard's rendered him chronically thin and weak for the remainder of his life, yet he methodically expanded his portfolio to over 200 entries, many developed during periods of relative remission that allowed intermittent laboratory work. This resilience stemmed from his conviction in the causal mechanics of rocket propulsion, undeterred by or bodily constraints, as evidenced by his progression from theoretical calculations to practical filings even as health demands confined much activity to Worcester-based studies.

Institutional Support and Experimental Beginnings

Smithsonian Sponsorship for Altitude Research

In 1916, Robert H. Goddard, then a physics professor at , submitted a detailed proposal to the outlining his theoretical work on for achieving extreme altitudes, emphasizing the potential to carry scientific instruments beyond the reach of balloons for atmospheric research. The proposal, dated September 27, 1916, derived from Goddard's earlier derivations of equations and calculations showing that multi-stage solid-propellant rockets could reach altitudes of up to 190 miles under ideal conditions, far surpassing existing sounding methods. Smithsonian Secretary Charles D. Walcott, advised by astrophysicist Charles G. Abbot, approved a grant of $5,000 from the Hodgkins Fund on January 5, 1917, to be disbursed over five years specifically for experimental altitude research using rockets as instrument carriers. This funding, equivalent to approximately $130,000 in 2023 dollars, marked the first institutional support for Goddard's rocketry efforts and enabled the construction of a test facility on the grounds of Clark University's Worcester, Massachusetts campus, including a launch tower and instrumentation for measuring rocket performance. Initial experiments focused on solid-fuel rockets with black powder propellants, achieving altitudes of several hundred feet while gathering data on thrust, stability, and payload capacity to validate theoretical predictions. The sponsorship emphasized practical applications for and upper-atmosphere , aligning with the Smithsonian's interest in advancing scientific beyond limitations, though Goddard's reports to the institution highlighted challenges like inconsistent propellant burning and structural failures in early static tests. By 1918, amid , Goddard demonstrated prototype rockets to the U.S. military under the grant's auspices, achieving velocities up to 500 feet per second, which informed refinements in and staging concepts. The funding's structure required annual progress reports, culminating in the Smithsonian's publication of Goddard's comprehensive report in 1920, which detailed the mathematical and experimental foundations of his altitude-reaching methods.

Development of the First Liquid-Fueled Rocket

Goddard initiated development of technology in September 1921, recognizing that liquids could provide higher exhaust velocities than solid propellants for greater efficiency in achieving altitude. Over the following years, he conducted static engine tests, culminating in a successful firing of a liquid-propellant motor by late 1925, which informed the design of his first flight-ready vehicle. Funded in part by a 1920 grant initially aimed at solid-fuel sounding rockets, Goddard adapted the project to liquids, employing gasoline as fuel and (LOX) as oxidizer; LOX was selected for its ability to vaporize at -297°F (-183°C), generating internal pressure to force propellants into the without complex pumps. The rocket's engine featured a top-mounted and , an unconventional configuration by later standards that placed the thrust vector above the tanks for structural simplicity, with vanes surrounding the for rudimentary guidance. feed relied on pressurized vapor from the and an auxiliary , augmented by a flap to prevent ; ignition was achieved via heads and in a simple starter system, with pre-launch pressurization assisted by an external oxygen cylinder. involved Goddard, his wife , and assistants including colleagues and machinist Nils Swenson, who fabricated components in a modest Worcester laboratory despite limited resources and technical challenges like managing cryogenic handling. An initial launch attempt on March 8, 1926, failed due to ignition issues, but on March 16, 1926, at his aunt Effie Wooster's farm in —a snowy field outside Worcester—Goddard successfully ignited the 10-foot-tall device, later dubbed "Nell." The rocket burned for approximately 2.5 seconds, accelerating to 60 (97 km/h), attaining a maximum altitude of 41 feet (12.5 meters), and landing 184 feet (56 meters) away after a brief, uncontrolled trajectory that ended in impact. Though modest in scale—the fueled weighed about 11 pounds (5 kg)—this event marked the world's first powered flight of a , validating Goddard's theoretical predictions from his 1919 Smithsonian paper and paving the way for iterative improvements in subsequent tests.

Military Demonstrations and Early Flights

In 1917, Robert H. Goddard began developing under contracts with the U.S. Army and Ordnance Department to create potential anti-aircraft weapons during . These efforts involved experiments with high-grade in 1-inch diameter rockets tested for applications. By September 1918, Goddard had presented designs to the Army , including tube-launched rockets. On November 7, 1918, he demonstrated a tube-launched using an improvised as the launching platform. A further demonstration occurred on , 1918, at the Proving Grounds before representatives of the armed services, showcasing the basic concept that later influenced the development of the . Following the war's end, Goddard's focus shifted to liquid-propellant systems, culminating in the world's first successful liquid-fueled flight on March 16, 1926, at a farm in , near Worcester. The 10-foot-tall , powered by gasoline and , ignited for 2.5 seconds, achieving a speed of approximately 60 miles per hour, an altitude of 41 feet, and landing 184 feet from the launch frame. This brief flight validated Goddard's theoretical work on liquid propulsion, though it remained experimental and secretive. Subsequent early flights in the Worcester area refined the design. On May 4, 1926, Goddard launched a with the motor positioned at the top, marking an iteration toward more stable configurations. Further tests, including the "Hoopskirt" on December 26, 1928, represented his third liquid-fuel flight, incorporating structural improvements but still limited by rudimentary guidance and propulsion reliability. These demonstrations highlighted persistent challenges such as vibration control and fuel efficiency, yet demonstrated progressive altitudes and velocities in controlled environments.

Publication, Skepticism, and Vindication

Release of "A Method of Reaching Extreme Altitudes"

In , Robert H. Goddard published his seminal A Method of Reaching Extreme Altitudes as Smithsonian Miscellaneous Collections, Volume 71, Number 2, following a $5,000 grant from the in January 1917 to investigate methods for elevating scientific instruments to extreme heights. The document, prefaced with a date of May 26, , synthesized Goddard's theoretical analyses and static tests conducted between 1917 and 1918, emphasizing solid- and liquid-propellant rockets as superior to lighter-than-air devices for surpassing 50,000 feet. The publication outlined Goddard's derivation of the rocket equation, calculating achievable velocities based on exhaust speed, , and staging efficiency, with projections for single-stage rockets reaching up to 15 miles and multi-stage designs potentially exceeding 120 miles under ideal conditions. It advocated liquid propellants like gasoline and for higher specific impulses, estimating requirements and structural optimizations, while addressing practical challenges such as design and atmospheric drag. Accompanied by 10 plates illustrating test apparatuses and theoretical diagrams, the 69-page marked the first comprehensive engineering treatment of rocketry for scientific altitudes, distributed by the Smithsonian to over 2,000 recipients including astronomers, physicists, and engineers worldwide. Goddard concluded the paper by speculating on interstellar applications, noting that a with near-perfect could theoretically reach the moon's distance of 239,000 miles, though he framed this as an rather than immediate feasibility. The release established Goddard's foundational contributions to rocketry theory, influencing subsequent developments in while prompting broader scientific discourse on viability, despite initial limited experimental validation.

Media Ridicule and the New York Times Editorial

Following the publication of Goddard's monograph A Method of Reaching Extreme Altitudes on January 5, 1920, by the , media coverage initially highlighted its potential for high-altitude research but quickly shifted to skepticism regarding interplanetary applications. The published an article on January 12, 1920, reporting on the Smithsonian's endorsement of Goddard's multi-stage rocket design for , but the subsequent editorial response exemplified broader dismissal. On January 13, 1920, the featured an unsigned editorial in its "Topics of the Times" column that derided Goddard's extrapolated vision of lunar travel via , titling it implicitly as straining credulity. The piece asserted that Goddard "seems to lack the knowledge ladled out daily in high schools" about Newton's third law of motion, erroneously claiming that a rocket could not propel itself in the of without "something better than a vacuum against which to react." This misrepresentation ignored the self-contained reaction mass expelled by the rocket's exhaust, a principle Goddard had correctly derived from first principles in his work. The editorial's tone amplified public and journalistic ridicule, portraying Goddard's ideas as fanciful and questioning his scientific competence despite his established experimental success with solid-fuel rockets. Other outlets echoed this sentiment, contributing to Goddard being mockingly dubbed "the Moon Man" in popular discourse, which deepened his aversion to and prompted greater in future endeavors. Goddard responded indirectly in a 1920 article, defending the physical feasibility of vacuum propulsion without directly confronting the press, emphasizing empirical validation over debate. This episode underscored prevailing scientific conservatism toward rocketry's extraterrestrial potential, prioritizing atmospheric applications while rejecting vacuum operations as implausible.

Long-Term Aftermath and Official Correction

Goddard's 1920 publication and the ensuing ridicule, including the editorial on January 13, 1920, which claimed that rockets could not function in the of due to a purported misunderstanding of Newton's third law, contributed to long-standing skepticism toward his work among some scientific and journalistic circles. This doubt persisted, exacerbating challenges in securing public funding and broader institutional support during his lifetime, as Goddard maintained secrecy around many innovations to protect patents amid perceived dismissal. Despite this, he continued private development until his death from throat cancer on August 10, 1945, at age 62, leaving behind over 200 patents, many filed posthumously. Posthumous vindication accelerated with the onset of the . In 1957, the Soviet Union's Sputnik launch highlighted practical rocketry achievements, drawing renewed attention to Goddard's foundational liquid-fuel designs and multi-stage concepts. By , the U.S. awarded him a posthumous , explicitly recognizing his "pioneering research in rocket propulsion" that underpinned modern developments. That same year, the established the in , naming it in his honor to commemorate his role as a pioneer of American rocketry. The most direct official correction of early skepticism came from the New York Times itself. On July 17, 1969—the day after the launch toward the Moon—the paper published a retraction of its 1920 editorial: "Further investigation and experimentation have confirmed the findings of in the and it is now definitely established that a can function in a . The 'Times' regrets the error." This acknowledgment, issued 49 years later amid humanity's first lunar mission, underscored Goddard's prescience and marked a symbolic reversal, affirming that his theoretical and experimental work had validated interplanetary rocketry long before widespread acceptance. His released papers and designs subsequently influenced U.S. and programs, cementing his legacy as the father of modern rocketry despite the initial professional isolation.

Private Funding and Major Advancements

Lindbergh's Role and Guggenheim Grants

, renowned for his 1927 solo , became intrigued by rocketry's potential for high-altitude aviation and propulsion advancements shortly thereafter. He met Goddard on November 23, 1929, at , where Goddard demonstrated his theoretical calculations and early solid-fuel rocket apparatus, convincing Lindbergh of the viability of liquid-propellant systems for extreme altitudes. Impressed, Lindbergh committed to aiding Goddard's efforts by seeking private funding, recognizing the limitations of institutional support amid the economic downturn following the 1929 stock market crash. Lindbergh directly approached philanthropist , a with prior investments in research through the Daniel Guggenheim Fund for the Promotion of . In July 1930, Guggenheim approved an initial two-year grant of $50,000 to , conditional on progress reports and with the potential for an additional $50,000 renewal, marking a significant shift from Goddard's prior modest Smithsonian allocations totaling around $10,000 by 1927. This funding, personally secured by Lindbergh's advocacy, enabled Goddard to establish a dedicated research team, acquire specialized materials, and conduct static tests without academic oversight. The grant was renewed in for another two years, bringing the total to —equivalent to approximately $1.8 million in 2025 dollars—sustained through Lindbergh's ongoing involvement and Goddard's detailed quarterly demonstrations of thrust chamber efficiency and designs. These Guggenheim resources proved pivotal, funding the transition to full-scale liquid-fueled engines using and , while Lindbergh's visits, including one on , 1935, reinforced the foundation's commitment by witnessing launch preparations. Absent this private patronage, Goddard's empirical progress in stabilizing and achieving multi-second burns would have stalled amid pervasive skepticism from established scientific bodies.

Relocation to Roswell and Variable-Thrust Innovations

In 1930, Robert H. Goddard relocated his rocketry research from to , facilitated by a $50,000 grant over five years from the Fund for the Promotion of Aeronautics. The selection of Roswell stemmed from its rural setting, which reduced risks to bystanders during test flights, and its arid climate, enabling consistent year-round operations unlike the variable weather in . Goddard established operations on a 6,000-acre leased for the purpose, where he and a small team constructed launch facilities, including a tower and blast deflectors, and conducted over 30 flights through 1941. During the Roswell period, Goddard pursued enhancements in design, with a key focus on achieving variable for improved control and efficiency. He developed motors capable of modulating output, incorporating high-speed turbopumps to regulate flow rates from and . Between September 1941 and July 1942, experiments tested refined combustion chambers and pump units specifically for variable- operation, addressing challenges in stable ignition and sustained modulation under varying loads. These efforts laid groundwork for throttleable engines, demonstrated in static tests that achieved controlled variations essential for applications like guided rocketry and eventual jet-assisted takeoff systems. Goddard's variable-thrust innovations involved mechanical feedback systems, such as spring-stabilized swivel mounts on engines, to maintain stability during adjustments, though full flight integration remained limited by material stresses and measurement precision of the era. By 1941, under emerging contracts, these prototypes informed practical liquid-propellant motors with adjustable , marking a departure from fixed-burn designs toward dynamically responsive . Despite secrecy constraints, the Roswell tests yielded data on efficiency at partial thrusts, contributing to Goddard's 214 patents, including those for propellant feed controls.

Record Flights, Data Analysis, and Technical Limitations

Goddard's team in Roswell conducted numerous test launches during , with fifty-six flights recorded between 1930 and 1941, of which seventeen exceeded 1,000 feet in altitude. A notable early success occurred on , 1935, when A-series A-5 achieved 4,800 feet (1,463 meters) in a 20-second flight, reaching speeds over 550 miles per hour (885 km/h) and traveling 13,000 feet (3,962 meters) downrange before deployment. Later efforts with L-series rockets, incorporating gyroscopic stabilization and thin-walled fuel tanks, culminated in a flight on August 9, 1938, reaching 3,294 feet, though overall program highs approached 7,500 feet (2,286 meters) and 2,400 meters in progressively refined designs. These records demonstrated feasibility of sustained liquid-propellant thrust but remained constrained below practical orbital thresholds due to iterative scaling issues. ![Goddard with one of his liquid-fueled rockets near the launch site in Roswell][float-right]
Data collection relied on ground-based tracking, relay-operated cameras capturing ascent phases, and post-flight recovery of instruments for and measurements. Goddard analyzed efficiency through vacuum-chamber tests and flight telemetry precursors, such as gauges and accelerometers, to correlate flow rates with altitude gains; for instance, experiments confirmed steady pumping of and mitigated imbalances, enabling speeds up to 500 mph in launches. His notebooks detailed causal factors like fuel vaporization and nozzle design, revealing that optimal required precise to avoid incomplete burns, with data iteratively refining engine clusters for variable output.
Technical limitations stemmed primarily from materials and control inadequacies inherent to . Thin-walled tanks wound with high-tensile wire reduced weight but risked rupture under vibration, while rudimentary gyroscopes provided marginal stability against aerodynamic torque, often resulting in erratic trajectories beyond 1,000 feet. Fuel pumping systems, dependent on gas-pressurized feeds rather than turbopumps, limited sustained high-thrust phases, capping altitudes as propellants depleted unevenly; cooling challenges in chambers led to frequent meltdowns after 20-30 seconds, as uncooled metals eroded under extreme temperatures exceeding 3,000°F. Guidance remained passive or pendulum-based, vulnerable to in Roswell's variable conditions, underscoring the need for active vanes and feedback loops that Goddard's protocols delayed sharing, hindering broader advancements. These constraints, rooted in empirical trial-and-error without computational aids, confined flights to subsonic, low-altitude proofs-of-concept despite theoretical designs projecting extreme reaches.

World War II Contributions and Secrecy

Annapolis Facility and Naval Research

In July 1942, shortly after the United States entered World War II, Robert H. Goddard relocated his rocket research team from Roswell, New Mexico, to the U.S. Naval Engineering Experiment Station in Annapolis, Maryland, to support naval ordnance development under contract with the Navy's Bureau of Aeronautics. The move integrated Goddard's expertise in liquid-propellant rocketry with the Navy's established rocket research group, which had initiated work on long-burning liquid engines earlier in 1941. At Annapolis, Goddard's team—comprising approximately 15 engineers and technicians—operated from a dedicated shop facility equipped for static testing, where they conducted over 200 engine firings by mid-1945. The primary focus was advancing reliable, controllable rocket motors for military applications, including jet-assisted takeoff () units to enable heavily loaded seaplanes and aircraft carriers to achieve flight from short decks or water surfaces. Goddard's innovations included refined variable-thrust engines using and , improved turbopumps for consistent fuel delivery, and gimbal-mounted nozzles with hydraulic actuators for , achieving stable burns exceeding 100 seconds duration and thrusts up to 1,000 pounds. These efforts built on pre-war designs but prioritized ruggedness for naval environments, with tests emphasizing corrosion-resistant materials and rapid-restart capabilities, though full-scale flight demonstrations were limited due to wartime secrecy and facility constraints. All research adhered to strict protocols, with results shared only within naval channels and Goddard's patents withheld from public disclosure to prevent enemy access. By early 1945, as Goddard's health deteriorated from throat cancer, the team had prototyped scalable engine clusters, but operational deployment lagged behind simpler solid-fuel alternatives favored by the military for immediacy. Goddard's Annapolis tenure ended with his death on August 10, 1945; the Navy briefly continued elements of his work before disbanding the group later that year, archiving data that influenced post-war programs despite limited wartime impact.

Secrecy Protocols and Patent Withholding

During World War II, Robert H. Goddard's research under contract with the U.S. Navy at the Naval Engineering Experiment Station in Annapolis, Maryland, was governed by stringent military secrecy protocols to prevent technological intelligence from reaching Axis powers. Assigned in 1941 to develop jet-assisted takeoff (JATO) units and variable-thrust liquid-propellant rocket motors for naval aircraft and potential weaponry, Goddard led a small team that achieved functional prototypes by 1943, including engines capable of throttling between 25% and 100% thrust using hydrogen peroxide decomposition. These efforts built on his pre-war innovations but operated under classified conditions, limiting dissemination even within U.S. military branches and requiring compartmentalized access among collaborators like his wife Esther and engineer assistants. The U.S. Patent and Trademark Office enforced a formal program under the of 1951's wartime predecessor authority, issuing over 11,000 secrecy orders from 1941 to 1945 on applications posing risks to , including rocketry and propulsion technologies. 's ongoing patent filings during this period—adding to his existing 214 rocketry-related patents—were subject to such orders, withholding public issuance and examination until rescinded post-war, typically years later. This prevented enemy exploitation, as evidenced by the absence of U.S. liquid-fuel rocket details in captured German documents, despite earlier public patents influencing pre-war German designs like the V-2. 's personal aversion to premature disclosure, rooted in prior experiences of idea appropriation without credit, reinforced compliance, though it frustrated potential Allied synergies. Postwar enabled partial release, but the delays contributed to litigation by Esther Goddard against the U.S. government in the , alleging infringement on withheld patents used in programs like the Army's missile without adequate compensation. The Court of Claims awarded $1.2 million in 1973 for 48 validated claims, underscoring how secrecy protocols preserved innovations at the cost of immediate inventor recognition and royalties. This wartime framework exemplified causal trade-offs in military R&D: short-term security gains versus long-term knowledge diffusion barriers, with Goddard's classified output directly informing U.S. post-1945 rocketry advancements despite limited wartime production scale.

Parallel German Developments and V-2 Comparisons

Parallel to Goddard's pioneering liquid-fueled rocket launch on March 16, 1926, German rocketry emerged through theoretical foundations laid by in his 1923 book Die Rakete zu den Planetenräumen, which proposed liquid-propellant multi-stage vehicles for space travel. The Verein für Raumschiffahrt (VfR), founded on July 5, 1927, conducted amateur liquid-fueled experiments, including the Repulsor series engines tested from 1930 onward, achieving brief powered flights with and mixtures akin to Goddard's propellants. These efforts mirrored Goddard's private, self-funded trials but benefited from a growing enthusiast community, though early VfR rockets remained small-scale and suborbital, reaching altitudes under 1 kilometer. By 1932, the German Army assumed control of rocketry under , recruiting to develop military applications, shifting from civilian exploration to weaponization with substantial state resources. The program progressed through prototypes: A-1 (1933, static tests), A-2 (1934, first coastal launches up to 2.2 km altitude), and larger designs culminating in the A-4 (V-2) at the research center established in 1937. The V-2 achieved its first successful vertical test flight on October 3, 1942, powered by a 25-ton-thrust using alcohol and , and entered combat deployment on September 8, 1944, against targets in and , attaining speeds over Mach 4 and ranges up to 320 km. This state-backed scaling contrasted sharply with Goddard's constrained wartime work at the Annapolis facility, where he focused on components and catapults without pursuing large vehicles. Technical comparisons reveal conceptual overlaps—both employed with volatile fuels, exhaust vanes for control, and gyroscopic stabilization—but fundamental differences in scale and execution. Goddard's 1930s Series A-F and L-C rockets measured 4-5 meters, generated 50-100 pounds of , and topped 762 meters altitude, emphasizing innovations like thin-walled tanks and variable- gimballing without . The V-2, at 14 meters and 56,000 pounds , incorporated a hydrogen-peroxide-driven for high flow rates, inertial guidance for ballistic trajectories, and supersonic , enabling it to reach the edge of (over 80 km apogee). While Goddard patented liquid-fuel concepts in 1914 and suspected German appropriation upon examining V-2 components in spring 1945, engineering analyses indicate independent evolution, with Germans drawing from public journals but devising pumps and structures via parallel logical progression rather than direct copying. Von Braun later acknowledged Goddard's publications as inspirational, yet the V-2's operational success stemmed from massive funding—equivalent to billions in modern terms—and forced labor, absent in Goddard's solitary endeavors.

Personal Character and Private Life

Family Dynamics and Marital Partnership

Robert H. Goddard was born on October 5, 1882, in , as the only surviving child of Danford Goddard, a who later worked as a bookkeeper, salesman, and machine-shop owner, and Fannie Louise Hoyt, his wife. The family's modest circumstances supported a genteel upbringing, with Goddard's parents encouraging his despite his frequent childhood illnesses, including and , which limited his formal schooling and deepened family bonds through home-based care and reading. Nahum's mechanical interests and Fannie's nurturing role fostered Goddard's early experiments with toys and kites, laying groundwork for his scientific pursuits, though no records indicate tensions or conflicts within the household. Fannie died in 1920, and in 1928, leaving Goddard without immediate family reliance as he advanced into independent research. On June 21, 1924, Goddard married Christine Kisk, a 23-year-old physics student and former secretary at whom he had met around 1919–1920 when she was 17 and working to fund her education at . Spanning a 19-year age difference, their union formed a dedicated professional and personal partnership, with Esther transitioning from administrative roles to hands-on collaboration, including photography of rocket tests, data documentation, and assistance in experiments during their moves to , and later , in 1930. The couple remained childless, prioritizing Goddard's secretive rocketry work amid his chronic health issues, which necessitated seclusion and limited social engagements. Esther's role extended beyond support to active contribution, as she operated cameras to capture launch sequences—essential for analysis in an era without advanced instrumentation—and managed logistics during field tests, demonstrating resilience in harsh conditions like New Mexico's desert environment. Their relationship, unmarred by public accounts of discord, centered on mutual commitment to Goddard's vision, with Esther's post-1945 efforts compiling and editing his 18,000-page papers for publication, ensuring preservation of his technical legacy until her death on June 4, 1982. This alliance exemplified a rare integration of marital and scientific collaboration, sustaining Goddard's isolation-driven focus without evident strain from his reclusive habits or professional setbacks.

Work Ethic, Isolation, and Psychological Resilience

Goddard demonstrated an exceptional work ethic through his single-minded dedication to rocketry, pursuing theoretical and experimental advancements with meticulous precision despite limited resources and frequent setbacks. His persistence was evident in the decades-long development of liquid-fueled rockets, where he conducted thousands of tests, refining designs iteratively even as early efforts yielded modest altitudes of mere feet. This drive stemmed from an early epiphany on March 16, 1899, when, as a 16-year-old, he envisioned multi-stage rockets reaching the moon, fueling a lifelong commitment undeterred by academic duties at Clark University or health constraints. His preference for isolation intensified after public ridicule, notably the 1920 New York Times editorial mocking his interplanetary ambitions as premature, which reinforced his innate shyness and aversion to collaboration. Goddard deliberately withheld details of his work from peers, opting to labor alone or with a small cadre of technicians to safeguard patents and ideas amid skepticism from scientific establishments. This solitary approach extended to relocations, such as to the remote , farm in the 1910s and later , in 1930, where arid conditions aided his frail health while minimizing external interference. Such seclusion, while enabling focused innovation, limited broader scientific discourse and funding opportunities until private patrons like intervened in 1929. Psychological resilience defined Goddard's character, as he overcame a near-fatal bout of diagnosed in March 1913, when physicians predicted death within weeks, yet recovered through rest and relocation to southern climates, resuming rigorous work by 1914. This iron will persisted against institutional dismissal and technical failures, with contemporaries noting his unflagging patience amid grant uncertainties and explosive mishaps; for instance, he endured recurrent lung issues into the 1940s while consulting for the on jet-assisted takeoff systems. His ability to compartmentalize adversity—channeling criticism into secrecy rather than abandonment—reflected a resilient rooted in empirical validation over popular opinion, ultimately validating his visions posthumously.

Final Years, Illness, and Death

In 1942, Goddard relocated his operations from , to the Naval Engineering Experimental Station in , to support wartime rocket development, a move that exposed him to a colder, more humid climate detrimental to his longstanding respiratory vulnerabilities stemming from contracted in 1913. Despite these challenges, he persisted with innovations, including variable-thrust engines and stabilization systems, until his health sharply declined in early 1945. A physician detected a malignant growth in Goddard's in May 1945, shortly after Germany's surrender, confirming a of cancer. He underwent two surgeries at the University of Hospital in an attempt to remove the tumor, but the cancer metastasized rapidly, leaving him able to communicate only in whispers and reliant on his wife, , to record his technical dictations. Goddard continued supervising experiments from his bedside until the end, prioritizing on and gyroscopic controls even as his condition worsened. Goddard died on August 10, 1945, at the age of 62 in , , succumbing to complications from the throat cancer. His remains were interred in Hope Cemetery, , his birthplace. At the time of his death, 131 of his 214 patented inventions remained unassigned, reflecting his focus on empirical validation over immediate commercialization.

Enduring Legacy and Critical Assessment

Direct Influence on Post-War Rocketry and Space Exploration

Following Robert H. Goddard's death on August 10, 1945, his widow Esther C. Goddard arranged for the release of his extensive technical notebooks, correspondence, and over 200 patents to U.S. government agencies, including the and the (NACA), providing detailed records of designs tested between 1926 and 1941. These documents outlined practical implementations of multi-stage rocketry, patented by Goddard in 1914 as a means to achieve greater altitudes through sequential staging, a principle directly incorporated into post-war U.S. missile systems like the Redstone and rockets developed under Wernher von Braun's team at the starting in 1950. Goddard's innovations in guidance and stability, including gyroscopically controlled vanes and swiveling engine mounts for —demonstrated in his 1930s Series A and L-C rockets—were patented and later adapted for attitude control in early American guided missiles and satellites, such as the program initiated in 1955 by the . His pioneering film cooling technique, which injected propellant along engine walls to prevent thermal damage, addressed overheating in liquid-fueled engines and influenced durable designs in subsequent launch vehicles, including those used by after its formation in 1958. In 1932, Goddard developed high-speed turbopumps to feed propellants under pressure, achieving reliable delivery rates that prefigured the in larger post-war engines, though scaled up from his experimental pumps delivering up to 7 gallons per minute of and oxygen. In 1958, Esther Goddard formally assigned 131 of his patents to the U.S. government without compensation, enabling direct access to proprietary designs for thrust chambers, nozzles, and vacuum performance validation—proven by Goddard in 1918 ground tests simulating space conditions. These elements informed NACA's early transition to , where they complemented imported German V-2 hardware by providing indigenous engineering precedents for reliable liquid propulsion, as acknowledged in 's post-Sputnik rocketry assessments. Von Braun, whose pre-war reading of Goddard's 1919 "A Method of Reaching Extreme Altitudes" shaped his multi-stage concepts, integrated similar staging and control ideas into U.S. programs after 1945, bridging European and American traditions despite Goddard's prior secrecy limiting wartime dissemination. However, immediate post-war scaling relied heavily on V-2-derived via , with Goddard's contributions manifesting more in refined, iterative U.S. developments than in foundational hardware assembly.

Honors, Craters, and Institutional Recognitions

The United States Congress authorized a Congressional Gold Medal for Goddard on September 16, 1959, via Public Law 86-277, posthumously honoring his foundational work in liquid-fueled rocketry and multi-stage rocket design that anticipated modern space propulsion. In 1960, the Smithsonian Institution awarded him the Langley Gold Medal posthumously, recognizing his pioneering theoretical and experimental advancements in rocket technology despite limited contemporary support. The United States Postal Service issued an 8-cent airmail stamp on October 5, 1964, featuring Goddard's portrait with an Atlas rocket and launch tower, commemorating his role as the father of American rocketry. NASA named its in , after him in May 1959, establishing the facility as a hub for space science, , and research that continues to operationalize principles derived from his early innovations. dedicated the Robert H. Goddard Library in 1969, honoring his tenure as a physics professor there from 1914 onward and his foundational patents developed during that period. 's , founded in 1961 at , was similarly named to acknowledge his prescient contributions to understanding atmospheric propulsion and potential interplanetary travel. The lunar crater , situated on the Moon's at coordinates approximately 21.0°S 147.7°W with a diameter of 104 kilometers, was officially named by the in recognition of his rocketry legacy. Asteroid 9252 , discovered in 1989, also bears his name, reflecting ongoing astronomical tributes to his empirical groundwork in and staged rocketry.

Overlooked Challenges: Government Neglect vs. Private Genius

Despite achieving the world's first liquid-fueled rocket launch on March 16, 1926, using gasoline and to reach an altitude of 41 feet, Robert H. Goddard received negligible support from the U.S. government throughout much of his career, compelling him to rely on personal resources and private . Early attempts to secure funding faltered; during , Goddard developed a solid-fuel rocket concept akin to the later for the U.S. Army , but post-Armistice in 1918, the warehoused the prototypes with minimal follow-through, leaving him feeling personally slighted by national neglect. Similarly, interwar overtures to the Army and other agencies met rebuffs, as officials dismissed rocketry's practical potential, forcing Goddard to fund initial experiments from his modest salary and small grants totaling around $12,750 over two decades. This governmental disinterest starkly contrasted with Goddard's resourceful private innovations, which advanced rocketry fundamentals without institutional backing. In 1929, aviator facilitated a pivotal grant from the Daniel and Florence Guggenheim Foundation, providing approximately $50,000 initially—equivalent to over $900,000 in 2025 dollars—for larger-scale research, enabling Goddard to establish a secluded testing site in , in 1930. There, operating with a small team including his wife as photographer and data recorder, he iteratively refined designs, achieving a single-stage altitude record of 2,346 feet on March 28, 1935, and incorporating gyroscopic stabilization and thin-walled fuel tanks for weight reduction—breakthroughs derived from first-hand experimentation rather than state-directed programs. The Guggenheims' cumulative support exceeded $200,000 by 1941, underscoring how private initiative sustained progress amid federal apathy, allowing Goddard to secure over 200 patents on multi-stage , , and . ![Dr. Goddard's launch tower at Roswell, NM, site of private rocket tests][float-right] The oversight extended to wartime priorities; even as Goddard offered expertise in the late 1930s, initial U.S. military responses remained tepid until 1942, when the Navy contracted him for variable-thrust engines in jet-assisted takeoff (JATO) units amid his declining health from tuberculosis. Posthumously, in 1945, the government recognized the infringement on his patents for wartime applications like the Bazooka anti-tank weapon and early missile systems, eventually settling with his estate for $1 million—the largest intellectual-property award of its kind at the time—affirming the foundational value of his privately driven genius. This delayed validation highlights an overlooked dynamic: American rocketry's origins stemmed not from public largesse but from individual perseverance against institutional skepticism, a pattern where private funding bridged gaps left by governmental short-sightedness until strategic imperatives demanded otherwise.

Cultural Depictions and Persistent Myths

Goddard appears in historical documentaries and television programs as a pioneering yet reclusive inventor whose ideas initially met with public and media skepticism. The National Aeronautics and Space Administration produced the 1961 film Dr. Robert H. Goddard - Father of Modern Rocketry, which recounts his development of liquid-fueled propulsion and early flight tests. Archival footage features in episodes of Impossible Engineering (2015), emphasizing his technical innovations like the 1926 launch of the world's first liquid-propellant rocket vehicle, which reached an altitude of 41 feet on March 16, 1926. In the Canadian series Murdoch Mysteries, Goddard's patents and rocketry concepts are invoked in fictional late-19th-century detective narratives to explore scientific feasibility. A 1964 United States airmail postage stamp, valued at 8 cents and issued on October 5, depicts Goddard with a multistage rocket, recognizing his foundational patents, including U.S. Patent 1,102,653 granted in 1914 for a solid-fuel rocket apparatus. Persistent myths exaggerate Goddard's isolation from the rocketry community, often citing the New York Times editorial of January 13, 1920, which claimed he ignored Newton's third law by proposing rockets function in a vacuum—a fundamental misunderstanding, as vacuum operation relies on internal reaction mass expulsion. The newspaper retracted this on July 20, 1969, post-Apollo 11, admitting ignorance of the topic; however, while such ridicule labeled him the "moon man," Goddard's 1919 Smithsonian pamphlet A Method of Reaching Extreme Altitudes actually spurred interest among international amateurs, including Soviet enthusiasts. Another misconception posits that German V-2 developers directly stole Goddard's designs, but archival reviews show his publications provided inspirational concepts like liquid fueling, yet the V-2's single-stage, alcohol-liquid oxygen engine and guidance systems evolved independently, uninfluenced by Goddard's unpublished multi-stage details or secretive testing protocols. This myth overlooks parallel developments by figures like Konstantin Tsiolkovsky and the causal role of Goddard's patent secrecy in limiting diffusion, prioritizing proprietary control over collaborative advancement.

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