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Apollo 14
Apollo 14
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Apollo 14
Alan Shepard and the American flag on the Moon, Apollo 14, February 1971 (photo by Edgar Mitchell)
Mission typeCrewed lunar landing (H)
OperatorNASA[1]
COSPAR ID
  • CSM: 1971-008A[2]
  • LM: 1971-008C[2]
SATCAT no.
Mission duration9 days, 1 minute, 58 seconds
Spacecraft properties
Spacecraft
ManufacturerCSM: North American Rockwell
LM: Grumman
Launch mass102,084 pounds (46,305 kg)
Landing mass11,481 pounds (5,208 kg)
Crew
Crew size3
Members
Callsign
  • CSM: Kitty Hawk
  • LM: Antares
Start of mission
Launch dateJanuary 31, 1971, 21:03:02 (1971-01-31UTC21:03:02Z) UTC
RocketSaturn V SA-509
Launch siteKennedy LC-39A
End of mission
Recovered byUSS New Orleans
Landing dateFebruary 9, 1971, 21:05:00 (1971-02-09UTC21:06Z) UTC
Landing siteSouth Pacific Ocean
27°1′S 172°39′W / 27.017°S 172.650°W / -27.017; -172.650 (Apollo 14 splashdown)
Orbital parameters
Reference systemSelenocentric
Periselene altitude16.9 kilometers (9.1 nmi)
Aposelene altitude108.9 kilometers (58.8 nmi)
Period120 minutes
Lunar orbiter
Spacecraft componentCommand and service module
Orbital insertionFebruary 4, 1971, 06:59:42 UTC
Orbital departureFebruary 7, 1971, 01:39:04 UTC
Orbits34
Lunar lander
Spacecraft componentLunar Module
Landing dateFebruary 5, 1971, 09:18:11 UTC
Return launchFebruary 6, 1971, 18:48:42 UTC
Landing siteFra Mauro
3°38′43″S 17°28′17″W / 3.64530°S 17.47136°W / -3.64530; -17.47136
Sample mass42.80 kilograms (94.35 lb)
Surface EVAs2
EVA duration
  • Total: 9 hours, 22 minutes, 31 seconds
  • 1st: 4 hours, 47 minutes, 50 seconds
  • 2nd: 4 hours, 34 minutes, 41 seconds
Docking with LM
Docking dateFebruary 1, 1971, 01:57:58 UTC
Undocking dateFebruary 5, 1971, 04:50:43 UTC
Docking with LM ascent stage
Docking dateFebruary 6, 1971, 20:35:52 UTC
Undocking dateFebruary 6, 1971, 22:48:00 UTC

Stuart Roosa, Alan Shepard, Edgar Mitchell

Apollo 14 (January 31 – February 9, 1971) was the eighth crewed mission in the United States Apollo program, the third to land on the Moon, and the first to land in the lunar highlands. It was the last of the "H missions", landings at specific sites of scientific interest on the Moon for two-day stays with two lunar extravehicular activities (EVAs or moonwalks).

The mission was originally scheduled for 1970, but was postponed because of the investigation following the failure of Apollo 13 to reach the Moon's surface, and the need for modifications to the spacecraft as a result. Commander Alan Shepard, Command Module Pilot Stuart Roosa, and Lunar Module Pilot Edgar Mitchell launched on their nine-day mission on Sunday, January 31, 1971, at 4:03:02 p.m. EST. En route to the lunar landing, the crew overcame malfunctions that might have resulted in a second consecutive aborted mission, and possibly, the premature end of the Apollo program.

Shepard and Mitchell made their lunar landing on February 5 in the Fra Mauro formation – originally the target of Apollo 13. During the two walks on the surface, they collected 94.35 pounds (42.80 kg) of Moon rocks and deployed several scientific experiments. To the dismay of some geologists, Shepard and Mitchell did not reach the rim of Cone crater as had been planned, though they came close. In Apollo 14's most famous event, Shepard hit two golf balls he had brought with him with a makeshift club.

While Shepard and Mitchell were on the surface, Roosa remained in lunar orbit aboard the Command and Service Module, performing scientific experiments and photographing the Moon, including the landing site of the future Apollo 16 mission. He took several hundred seeds on the mission, many of which were germinated on return, resulting in the so-called Moon trees, that were widely distributed in the following years. After liftoff from the lunar surface and a successful docking, the spacecraft was flown back to Earth where the three astronauts splashed down safely in the Pacific Ocean on February 9.

Astronauts and key Mission Control personnel

[edit]
Position Astronaut
Commander Alan B. Shepard Jr.
Second and last spaceflight
Command Module Pilot Stuart A. Roosa
Only spaceflight
Lunar Module Pilot Edgar D. Mitchell
Only spaceflight

The mission commander of Apollo 14, Alan Shepard, one of the original Mercury Seven astronauts, became the first American to enter space with a suborbital flight on May 5, 1961.[5] Thereafter, he was grounded by Ménière's disease, a disorder of the ear, and served as Chief Astronaut, the administrative head of the Astronaut Office. He had experimental surgery in 1968 which was successful and allowed his return to flight status.[6] Shepard, at age 47, was the oldest U.S. astronaut to fly when he made his trip aboard Apollo 14, and he is the oldest person to walk on the Moon.[7][8][9]

Apollo 14's Command Module Pilot (CMP), Stuart Roosa, aged 37 when the mission flew, had been a smoke jumper before joining the Air Force in 1953. He became a fighter pilot and then in 1965 successfully completed Aerospace Research Pilot School (ARPS) at Edwards Air Force Base in California prior to his selection as a Group 5 astronaut the following year.[10] He served as a capsule communicator (CAPCOM) for Apollo 9.[11] The Lunar Module Pilot (LMP), Edgar Mitchell, aged 40 at the time of Apollo 14, joined the Navy in 1952 and served as a fighter pilot, beginning in 1954. He was assigned to squadrons aboard aircraft carriers before returning to the United States to further his education while in the Navy, also completing the ARPS prior to his selection as a Group 5 astronaut.[12] He served on the support crew for Apollo 9 and was the LMP of the backup crew for Apollo 10.[13]

Shepard and his crew had originally been designated by Deke Slayton, Director of Flight Crew Operations and one of the Mercury Seven, as the crew for Apollo 13. NASA's management felt that Shepard needed more time for training given he had not flown in space since 1961, and chose him and his crew for Apollo 14 instead. The crew originally designated for Apollo 14, Jim Lovell as the commander, Ken Mattingly as CMP and Fred Haise as LMP, all of whom had backed up Apollo 11, was made the prime crew for Apollo 13 instead.[14][15]

Mitchell's commander on the Apollo 10 backup crew had been another of the original seven, Gordon Cooper, who had tentatively been scheduled to command Apollo 13, but according to author Andrew Chaikin, his casual attitude toward training resulted in him being not selected.[16] Also on that crew, but excluded from further flights, was Donn Eisele, likely because of problems aboard Apollo 7, which he had flown, and because he had been involved in a messy divorce.[14]

Apollo 14's backup crew was Eugene A. Cernan as commander, Ronald E. Evans Jr. as CMP and Joe H. Engle as LMP.[17] The backup crew, with Harrison Schmitt replacing Engle, would become the prime crew of Apollo 17.[18] Schmitt flew instead of Engle because there was intense pressure on NASA to fly a scientist to the Moon (Schmitt was a geologist) and Apollo 17 was the last lunar flight.[19] Engle, who had flown the X-15 to the edge of outer space, flew into space for NASA in 1981 on STS-2, the second Space Shuttle flight.[20]

During projects Mercury and Gemini, each mission had a prime and a backup crew. Apollo 9 commander James McDivitt believed meetings that required a member of the flight crew were being missed, so for Apollo a third crew of astronauts was added, known as the support crew.[21] Usually low in seniority, support crew members assembled the mission's rules, flight plan, and checklists, and kept them updated;[22][23] for Apollo 14, they were Philip K. Chapman, Bruce McCandless II, William R. Pogue and C. Gordon Fullerton.[9] CAPCOMs, the individuals in Mission Control responsible for communications with the astronauts were Evans, McCandless, Fullerton and Haise. A veteran of Apollo 13, which had aborted before reaching the Moon, Haise put his training for that mission to use, especially during the EVAs, since both missions were targeted at the same place on the Moon.[24] Had Haise walked on the Moon, he would have been the first Group 5 astronaut to do so, an honor that went to Mitchell.[25]

The flight directors during Apollo had a one-sentence job description, "The flight director may take any actions necessary for crew safety and mission success."[26] For Apollo 14, they were: Pete Frank, Orange team; Glynn Lunney, Black team; Milt Windler, Maroon team and Gerry Griffin, Gold team.[9]

Preparation and training

[edit]
Shepard in front of the Lunar Landing Research Vehicle, flown to simulate the landing

Prime and backup crews for both Apollo 13 and 14 were announced on August 6, 1969.[27] Apollo 14 was scheduled for July 1970, but in January of that year, due to budget cuts that saw the cancellation of Apollo 20, NASA decided there would be two Apollo missions per year with 1970 to see Apollo 13 in April and Apollo 14 likely in October or November.[28]

The investigation into the accident which caused an abort of Apollo 13 delayed Apollo 14. On May 7, 1970, NASA Administrator Thomas O. Paine announced that Apollo 14 would launch no earlier than December 3, and the landing would be close to the site targeted by Apollo 13. The Apollo 14 astronauts continued their training.[29] On June 30, 1970, following the release of the accident report and a NASA review of what changes to the spacecraft would be necessary, NASA announced that the launch would slip to no earlier than January 31, 1971.[30]

The crew of Apollo 14 trained together for 19 months after assignment to the mission, longer than any other Apollo crew to that point.[31] In addition to the normal training workload, they had to supervise the changes to the command and service module (CSM) made as a result of the Apollo 13 investigation, much of which was delegated by Shepard to Roosa.[32] Mitchell later stated, "We realized that if our mission failed—if we had to turn back—that was probably the end of the Apollo program. There was no way NASA could stand two failures in a row. We figured there was a heavy mantle on our shoulders to make sure we got it right."[33]

Before the abort of the Apollo 13 mission, the plan was to have Apollo 14 land near Littrow crater, in Mare Serenitatis, where there are features that were thought to be volcanic. After Apollo 13 returned, it was decided that its landing site, near Cone crater in the Fra Mauro formation, was scientifically more important than Littrow. The Fra Mauro formation is composed of ejecta from the impact event that formed Mare Imbrium, and scientists hoped for samples that originated deep under the Moon's surface. Cone crater was the result of a young, deep impact, and large enough to have torn through whatever debris was deposited since the Imbrium Event, which geologists hoped to be able to date. Landing at Fra Mauro would also allow orbital photography of another candidate landing site, the Descartes Highlands, which became the landing site for Apollo 16. Although Littrow went unvisited, a nearby area, Taurus-Littrow, was the landing site for Apollo 17.[34] Apollo 14's landing site was located slightly closer to Cone crater than the point designated for Apollo 13.[35]

The change in landing site from Littrow to Fra Mauro affected the geological training for Apollo 14. Before the switch, the astronauts had been taken to volcanic sites on Earth; afterwards, they visited crater sites, such as the Ries Crater in West Germany and an artificial crater field created for astronaut training in Arizona's Verde Valley. The effectiveness of the training was limited by a lack of enthusiasm shown by Shepard, which set the tone for Mitchell. Harrison Schmitt suggested that the commander had other things on his mind, such as overcoming a ten-year absence from spaceflight and ensuring a successful mission after the near-disaster of Apollo 13.[36]

Shepard (left) and Mitchell during geological training

Roosa undertook training for his period alone in lunar orbit, when he would make observations of the Moon and take photographs. He had been impressed by the training given to Apollo 13 prime crew CMP Mattingly by geologist Farouk El-Baz and got El-Baz to agree to undertake his training. The two men pored over lunar maps depicting the areas the CSM would pass over. When Shepard and Mitchell were on their geology field trips, Roosa would be overhead in an airplane taking photographs of the site and making observations. El-Baz had Roosa make observations while flying his T-38 jet at a speed and altitude simulating the speed at which the lunar surface would pass below the CSM.[37]

Another issue that had marked Apollo 13 was the last-minute change of crew due to exposure to communicable disease.[38] To prevent another such occurrence, for Apollo 14 NASA instituted what was called the Flight Crew Health Stabilization Program. Beginning 21 days before launch, the crew lived in quarters at the launch site, Florida's Kennedy Space Center (KSC), with their contacts limited to their spouses, the backup crew, mission technicians, and others directly involved in training. Those individuals were given physical examinations and immunizations, and crew movements were limited as much as possible at KSC and nearby areas.[39]

The Command and Service Modules were delivered to KSC on November 19, 1969; the ascent stage of the LM arrived on November 21 with the descent stage three days later. Thereafter, checkout, testing and equipment installation proceeded.[40] The launch vehicle stack, with the spacecraft on top, was rolled out from the Vehicle Assembly Building to Pad 39A on November 9, 1970.[41]

Hardware

[edit]

Spacecraft

[edit]
The Apollo 14 launch vehicle is rolled out from the Vehicle Assembly Building, November 9, 1970.

The Apollo 14 spacecraft consisted of Command Module (CM) 110 and Service Module (SM) 110 (together CSM-110), called Kitty Hawk, and Lunar Module 8 (LM-8), called Antares.[42] Roosa had chosen the CSM's call sign after the town in North Carolina where, in 1903, the Wright Brothers first flew their Wright Flyer airplane (also known as Kitty Hawk). Antares was named by Mitchell after the star in the constellation Scorpius that the astronauts in the LM would use to orient the craft for its lunar landing.[43][44][45] Also considered part of the spacecraft were a Launch Escape System and a Spacecraft/Launch Vehicle Adapter,[46] numbered SLA-17.[47]

The changes to the Apollo spacecraft between Apollo 13 and 14 were more numerous than with earlier missions, not only because of the problems with Apollo 13, but because of the more extensive lunar activities planned for Apollo 14.[42] The Apollo 13 accident had been caused by the explosive failure of an oxygen tank, after the insulation of the internal wiring had been damaged by heating of the tank contents pre-launch—that the oxygen had gotten hot enough to damage the insulation had not been realized, since the protective thermostatic switches had failed because they were, through an error, not designed to handle the voltage applied during ground testing. The explosion damaged the other tank or its tubing, causing its contents to leak away.[48]

The changes in response included a redesign of the oxygen tanks, with the thermostats being upgraded to handle the proper voltage.[49] A third tank was also added, placed in Bay 1 of the SM, on the side opposite the other two, and was given a valve that could isolate it in an emergency, and allow it to feed the CM's environmental system only. The quantity probe in each tank was upgraded from aluminum to stainless steel.[50]

Also in response to the Apollo 13 accident, the electrical wiring in Bay 4 (where the explosion had happened) was sheathed in stainless steel. The fuel cell oxygen supply valves were redesigned to isolate the Teflon-coated wiring from the oxygen. The spacecraft and Mission Control monitoring systems were modified to give more immediate and visible warnings of anomalies.[49] The Apollo 13 astronauts had suffered shortages of water and of power after the accident.[51] Accordingly, an emergency supply of 5 US gallons (19 L; 4.2 imp gal) of water was stored in Apollo 14's CM, and an emergency battery, identical to those that powered the LM's descent stage, was placed in the SM. The LM was modified to make the transfer of power from LM to CM easier.[52]

Other changes included the installation of anti-slosh baffles in the LM descent stage's propellant tanks. This would prevent the low fuel light from coming on prematurely, as had happened on Apollo 11 and 12. Structural changes were made to accommodate the equipment to be used on the lunar surface, including the Modular Equipment Transporter.[53]

Launch vehicle

[edit]

The Saturn V used for Apollo 14 was designated SA-509, and was similar to those used on Apollo 8 through 13.[54] At 6,505,548 pounds (2,950,867 kg), it was the heaviest vehicle yet flown by NASA, 3,814 pounds (1,730 kg) heavier than the launch vehicle for Apollo 13.[55]

A number of changes were made to avoid pogo oscillations, that had caused an early shutdown of the center J-2 engine on Apollo 13's S-II second stage. These included a helium gas accumulator installed in the liquid oxygen (LOX) line of the center engine, a backup cutoff device for that engine, and a simplified 2-position propellant utilization valve on each of the five J-2 engines.[56]

ALSEP and other lunar surface equipment

[edit]

The Apollo Lunar Surface Experiments Package (ALSEP) array of scientific instruments carried by Apollo 14 consisted of the Passive Seismic Experiment (PSE), Active Seismic Experiment (ASE), Suprathermal Ion Detector Experiment (SIDE), Cold Cathode Ion Gauge Experiment (CCIG), and Charged Particle Lunar Environment Experiment (CPLEE). Two additional lunar surface experiments not part of the ALSEP were also flown, the Laser Ranging Retroreflector (LRRR or LR3), to be deployed in the ALSEP's vicinity, and the Lunar Portable Magnetometer (LPM), to be used by the astronauts during their second EVA.[57] The PSE had been flown on Apollo 12 and 13, the ASE on Apollo 13, the SIDE on Apollo 12, the CCIG on Apollo 12 and 13, and the LRRR on Apollo 11. The LPM was new, but resembled equipment flown on Apollo 12.[58] The ALSEP components flown on Apollo 13 were destroyed when its LM burned up in Earth's atmosphere.[59] Deployment of the ALSEP, and of the other instruments, each formed one of Apollo 14's mission objectives.[57]

A close-up view of the Apollo 14 ALSEP Central Station deployed on the Moon

The PSE was a seismometer, similar to one left on the Moon by Apollo 12, and was to measure seismic activity in the Moon. The Apollo 14 instrument would be calibrated by the impact, after being jettisoned, of the LM's ascent stage, since an object of known mass and velocity would be impacting at a known location on the Moon. The Apollo 12 instrument would also be activated by the spent Apollo 14 S-IVB booster, which would impact the Moon after the mission entered lunar orbit. The two seismometers would, in combination with those left by later Apollo missions, constitute a network of such instruments at different locations on the Moon.[60]

The ASE would also measure seismic waves. It consisted of two parts. In the first, one of the crew members would deploy three geophones at distances up to 310 feet (94 m) from the ALSEP's Central Station, and on his way back from the furthest, fire thumpers every 15 feet (4.6 m). The second consisted of four mortars (with their launch tubes), of different properties and set to impact at different distances from the experiment. It was hoped that the waves generated from the impacts would provide data about seismic wave transmission in the Moon's regolith. The mortar shells were not to be fired until the astronauts had returned to Earth,[61] and in the event were never fired for fear they would damage other experiments. A similar experiment was successfully deployed, and the mortars launched, on Apollo 16.[62]

The LPM was to be carried during the second EVA and used to measure the Moon's magnetic field at various points.[63] The SIDE measured ions on the lunar surface, including from the solar wind. It was combined with the CCIG, which was to measure the lunar atmosphere and detect if it varied over time. The CPLEE measured the particle energies of protons and electrons generated by the Sun that reached the lunar surface.[64] The LRRR acts as a passive target for laser beams, allowing the measurement of the Earth/Moon distance and how it changes over time.[65] The LRRRs from Apollo 11, 14 and 15 are the only experiments left on the Moon by the Apollo astronauts that are still returning data.[66]

Flown for the first time on Apollo 14 was the Buddy Secondary Life Support System (BSLSS), a set of flexible hoses that would enable Shepard and Mitchell to share cooling water should one of their Primary Life Support System (PLSS) backpacks fail. In such an emergency, the astronaut with the failed equipment would get oxygen from his Oxygen Purge System (OPS) backup cylinder, but the BSLSS would ensure he did not have to use oxygen for cooling, extending the life of the OPS.[67] The OPSs used on Apollo 14 were modified from those used on previous missions in that the internal heaters were removed as unnecessary.[68]

Water bags were also taken to the lunar surface, dubbed "Gunga Dins", for insertion in the astronauts' helmets, allowing them sips of water during the EVAs.[67] These had been flown on Apollo 13, but Shepard and Mitchell were the first to use them on the Moon.[69] Similarly, Shepard was the first on the lunar surface to wear a spacesuit with commander's stripes: red stripes on arms, legs, and on the helmet, though one had been worn by Lovell on Apollo 13. These were instituted because of the difficulty in telling one spacesuited astronaut from the other in photographs.[70]

Modular Equipment Transporter

[edit]
Shepard and the Modular Equipment Transporter

The Modular Equipment Transporter (MET) was a two-wheeled handcart, used only on Apollo 14, intended to allow the astronauts to take tools and equipment with them, and store lunar samples, without needing to carry them. On later Apollo program missions, the self-propelled Lunar Roving Vehicle (LRV) was flown instead.[71]

The MET, when deployed for use on the lunar surface, was about 86 inches (220 cm) long, 39 inches (99 cm) wide and 32 inches (81 cm) high. It had pressurized rubber tires 4 inches (10 cm) wide and 16 inches (41 cm) in diameter, containing nitrogen and inflated to about 1.5 pounds per square inch (10 kPa).[72] The first use of tires on the Moon, these were developed by Goodyear and were dubbed their XLT (Experimental Lunar Tire) model. Fully loaded, the MET weighed about 165 pounds (75 kg).[73] Two legs combined with the wheels to provide four-point stability when at rest.[72]

Mission highlights

[edit]
Launch of Apollo 14

Launch and flight to lunar orbit

[edit]

Apollo 14 launched from Launch Complex 39-A at KSC at 4:03:02 pm (21:03:02 UTC), January 31, 1971.[42] This followed a launch delay due to weather of 40 minutes and 2 seconds; the first such delay in the Apollo program. The original planned time, 3:23 pm, was at the very start of the launch window of just under four hours; had Apollo 14 not launched during it, it could not have departed until March. Apollo 12 had launched during poor weather and twice been struck by lightning, as a result of which the rules had been tightened. Among those present to watch the launch were U.S. Vice President Spiro T. Agnew and the Prince of Spain, the future King Juan Carlos I.[42][55] The mission would take a faster trajectory to the Moon than planned, and thus make up the time in flight. Because it had, just over two days after launch, the mission timers would be put ahead by 40 minutes and 3 seconds so that later events would take place at the times scheduled in the flight plan.[74]

After the vehicle reached orbit, the S-IVB third stage shut down, and the astronauts performed checks of the spacecraft before restarting the stage for translunar injection (TLI), the burn that placed the vehicle on course for the Moon. After TLI, the CSM separated from the S-IVB, and Roosa performed the transposition maneuver, turning it around in order to dock with the LM before the entire spacecraft separated from the stage. Roosa, who had practiced the maneuver many times, hoped to break the record for the least amount of propellant used in docking. But when he gently brought the modules together, the docking mechanism would not activate. He made several attempts over the next two hours, as mission controllers huddled and sent advice. If the LM could not be extracted from its place on the S-IVB, no lunar landing could take place, and with consecutive failures, the Apollo program might end.[75] Mission Control proposed that they try it again with the docking probe retracted, hoping the contact would trigger the latches. This worked, and within an hour the joined spacecraft had separated from the S-IVB.[76] The stage was set on a course to impact the Moon, which it did just over three days later, causing the Apollo 12 seismometer to register vibrations for over three hours.[77]

The crew settled in for its voyage to Fra Mauro. At 60:30 Ground Elapsed Time, Shepard and Mitchell entered the LM to check its systems; while there they photographed a wastewater dump from the CSM, part of a particle contamination study in preparation for Skylab.[77] Two midcourse corrections were performed on the translunar coast, with one burn lasting 10.19 seconds and one lasting 0.65 seconds.[78]

Lunar orbit and descent

[edit]
Antares as seen from Kitty Hawk

At 81:56:40.70 into the mission (February 4 at 1:59:43 am EST; 06:59:43 UTC), the Service Propulsion System engine in the SM was fired for 370.84 seconds to send the craft into a lunar orbit with apocynthion of 169 nautical miles (313 km; 194 mi) and pericynthion of 58.1 nautical miles (107.6 km; 66.9 mi). A second burn, at 86:10:52 mission time, sent the spacecraft into an orbit of 58.8 nautical miles (108.9 km; 67.7 mi) by 9.1 nautical miles (16.9 km; 10.5 mi). This was done in preparation for the release of the LM Antares. Apollo 14 was the first mission on which the CSM propelled the LM to the lower orbit—though Apollo 13 would have done so had the abort not already occurred. This was done to increase the amount of hover time available to the astronauts, a safety factor since Apollo 14 was to land in rough terrain.[78]

After separating from the command module in lunar orbit, the LM Antares had two serious problems. First, the LM computer began getting an ABORT signal from a faulty switch. NASA believed the computer might be getting erroneous readings like this if a tiny ball of solder had shaken loose and was floating between the switch and the contact, closing the circuit. The immediate solution – tapping on the panel next to the switch – did work briefly, but the circuit soon closed again. If the problem recurred after the descent engine fired, the computer would think the signal was real and would initiate an auto-abort, causing the ascent stage to separate from the descent stage and climb back into orbit. NASA and the software teams at the Massachusetts Institute of Technology scrambled to find a solution. The software was hard-wired, preventing it from being updated from the ground. The fix made it appear to the system that an abort had already happened, and it would ignore incoming automated signals to abort. This would not prevent the astronauts from piloting the ship, though if an abort became necessary, they might have to initiate it manually.[79] Mitchell entered the changes with minutes to go until planned ignition.[80]

A second problem occurred during the powered descent, when the LM landing radar failed to lock automatically onto the Moon's surface, depriving the navigation computer of vital information on the vehicle's altitude and vertical descent speed. After the astronauts cycled the landing radar breaker, the unit successfully acquired a signal near 22,000 feet (6,700 m). Mission rules required an abort if the landing radar was out at 10,000 feet (3,000 m), though Shepard might have tried to land without it. With the landing radar, Shepard steered the LM to a landing which was the closest to the intended target of the six missions that landed on the Moon.[81]

Lunar surface operations

[edit]
Panorama of the Apollo 14 landing site taken in 1971

Shepard stated, after stepping onto the lunar surface, "And it's been a long way, but we're here."[82] The first EVA began at 9:42 am EST (14:42 UTC) on February 5, 1971, having been delayed by a problem with the communications system which set back the start of the first EVA to five hours after landing. The astronauts devoted much of the first EVA to equipment offloading, deployment of the ALSEP and the US flag,[83] as well as setting up and loading the MET. These activities were televised back to Earth, though the picture tended to degenerate during the latter portion of the EVA.[84] Mitchell deployed the ASE's geophone lines, unreeling and emplacing the two 310 feet (94 m) lines leading out from the ALSEP's Central Station. He then fired the thumper explosives, vibrations from which would give scientists back on Earth information about the depth and composition of the lunar regolith. Of the 21 thumpers,[85] five failed to fire.[84] On the way back to the LM, the astronauts collected and documented lunar samples, and took photographs of the area.[83] The first EVA lasted 4 hours, 47 minutes, 50 seconds.[84]

Mitchell studies a map while on the Moon.

The astronauts had been surprised by the undulating ground, expecting flatter terrain in the area of the landing, and this became an issue on the second EVA, as they set out, MET in tow, for the rim of Cone crater. The craters that Shepard and Mitchell planned to use for navigational landmarks looked very different on the ground than on the maps they had, based on overhead shots taken from lunar orbit. Additionally, they consistently overestimated the distance they travelled. Mission Control and the CAPCOM, Fred Haise, could see nothing of this, as the television camera remained near the LM, but they worried as the clock ticked on the EVA, and monitored the heavy breathing and rapid heartbeats of the astronauts. They topped one ridge that they expected was the crater rim, only to view more such terrain beyond. Although Mitchell strongly suspected the rim was nearby, they had become physically exhausted from the effort. They were then instructed by Haise to sample where they were and then start moving back towards the LM. Later analysis using the pictures they took determined that they had come within about 65 feet (20 m) of the crater's rim.[86][87] Images from the Lunar Reconnaissance Orbiter (LRO) show the tracks of the astronauts and the MET come to within 30 m of the rim.[88] The difficulties faced by Shepard and Mitchell would emphasize the need for a means of transportation on the lunar surface with a navigation system, which was met by the Lunar Roving Vehicle, already planned to fly on Apollo 15.[89]

Once the astronauts returned to the vicinity of the LM and were again within view of the television camera, Shepard performed a stunt he had been planning for years in the event he reached the Moon, and which is probably what Apollo 14 is best remembered for.[90] Shepard brought along a Wilson six iron golf club head, which he had modified to attach to the handle of the contingency sample tool, and two golf balls.[91] Shepard took several one-handed swings (due to the limited flexibility of the EVA suit) and exuberantly exclaimed that the second ball went "miles and miles and miles" in the low lunar gravity.[92] Mitchell then threw a lunar scoop handle as if it were a javelin. The "javelin" and one of the golf balls wound up in a crater together, with Mitchell's projectile a bit further. In an interview with Ottawa Golf, Shepard stated the other landed near the ALSEP.[93] The second EVA lasted 4 hours, 34 minutes, 41 seconds.[94] Shepard brought back the club, gave it to the USGA Museum in New Jersey, and had a replica made which he gave to the National Air and Space Museum.[95] In February 2021, to commemorate Apollo 14's 50th anniversary, imaging specialist Andy Saunders, who had previously worked to produce the clearest image of Neil Armstrong on the Moon, produced new, digitally enhanced images that were used to estimate the final resting places of the two balls that Shepard hit - the first landed approximately 24 yards from the "tee", while the second managed 40 yards.[96]

Lunar surface television showing Shepard taking a couple of golf swings

Lunar samples

[edit]
The "Big Bertha" rock (Lunar Sample 14321) was the third largest rock collected during the Apollo program.

A total of 94 pounds (43 kg) of Moon rocks, or lunar samples, were brought back from Apollo 14. Most are breccias, which are rocks composed of fragments of other, older rocks. Breccias form when the heat and pressure of meteorite impacts fuse small rock fragments together. There were a few basalts that were collected in this mission in the form of clasts (fragments) in breccia. The Apollo 14 basalts are generally richer in aluminum and sometimes richer in potassium than other lunar basalts. Most lunar mare basalts collected during the Apollo program were formed from 3.0 to 3.8 billion years ago. The Apollo 14 basalts were formed 4.0 to 4.3 billion years ago, older than the volcanism known to have occurred at any of the mare locations reached during the Apollo program.[97]

Some geologists were pleased enough with the close approach to Cone crater to send a case of scotch to the astronauts while they were in post-mission quarantine, though their enthusiasm was tempered by the fact that Shepard and Mitchell had documented few of the samples they brought back, making it hard and sometimes impossible to discern where they came from.[98] Others were less happy; Don Wilhelms wrote in his book on the geological aspects of Apollo, "the golf game did not set well with most geologists in light of the results at Cone crater. The total haul from the rim-flank of Cone ... was 16 Hasselblad photographs (out of a mission total of 417), six rock-size samples heavier than 50 g, and a grand total of 10 kg of samples, 9 kg of which are in one rock (sample 14321 [i.e., Big Bertha]). That is to say, apart from 14321 we have less than 1 kg of rock—962 g to be exact—from what in my opinion is the most important single point reached by astronauts on the Moon."[90] Geologist Lee Silver stated, "The Apollo 14 crews did not have the right attitude, did not learn enough about their mission, had the burden of not having the best possible preflight photography, and they weren't ready."[99] In their sourcebook on Apollo, Richard W. Orloff and David M. Harland doubted that if Apollo 13 had reached the Moon, Lovell, and Haise, given a more distant landing point, could have got as close to Cone crater as Shepard and Mitchell did.[35]

In January 2019 research showed that Big Bertha, which weighs 19.837 pounds (8.998 kg), has characteristics that make it likely to be a terrestrial (Earth) meteorite. Granite and quartz, which are commonly found on Earth but very rarely found on the Moon, were confirmed to exist on Big Bertha. To find the sample's age, the research team from Curtin University looked at bits of the mineral zircon embedded in its structure. "By determining the age of zircon found in the sample, we were able to pinpoint the age of the host rock at about four billion years old, making it similar to the oldest rocks on Earth," researcher Alexander Nemchin said, adding that "the chemistry of the zircon in this sample is very different from that of every other zircon grain ever analyzed in lunar samples, and remarkably similar to that of zircons found on Earth." This would mean Big Bertha is both the first discovered terrestrial meteorite and the oldest known Earth rock.[100][101]

Lunar orbit operations

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Kitty Hawk in lunar orbit

Roosa spent almost two days alone aboard Kitty Hawk, performing the first intensive program of scientific observation from lunar orbit, much of which was intended to have been done by Apollo 13.[102] After Antares separated and its crew began preparations to land, Roosa in Kitty Hawk performed an SPS burn to send the CSM to an orbit of approximately 60 nautical miles (110 km; 69 mi), and later a plane change maneuver to compensate for the rotation of the Moon.[103]

Roosa took pictures from lunar orbit. The Lunar Topographic Camera, also known as the Hycon camera, was supposed to be used to image the surface, including the Descartes Highlands site being considered for Apollo 16, but it quickly developed a fault with the shutter that Roosa could not fix despite considerable help from Houston. Although about half of the photographic targets had to be scrubbed, Roosa was able to obtain photographs of Descartes with a Hasselblad camera and confirm that it was a suitable landing point. Roosa also used the Hasselblad to take photographs of the impact point of Apollo 13's S-IVB near Lansburg B crater.[104][105] After the mission, troubleshooting found a tiny piece of aluminum contaminating the shutter control circuit, which caused the shutter to operate continuously.[106]

Roosa was able to see sunlight glinting off Antares and view its lengthy shadow on the lunar surface on Orbit 17; on Orbit 29 he could see the sun reflecting off the ALSEP.[107] He also took astronomical photographs, of the Gegenschein, and of the Lagrangian point of the Sun-Earth system that lies beyond the Earth (L2), testing the theory that the Gegenschein is generated by reflections off particles at L2. Performing the bistatic radar experiment, he also focused Kitty Hawk's VHF and S-band transmitters at the Moon so that they would bounce off and be detected on Earth in an effort to learn more about the depth of the lunar regolith.[94][108]

Return, splashdown and quarantine

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Apollo 14 landing in the South Pacific

Antares lifted off from the Moon at 1:48:42 pm EST[42] (18:48:42 UTC) on February 6, 1971. Following the first direct (first orbit) rendezvous on a lunar landing mission, docking took place an hour and 47 minutes later. Despite concerns based on the docking problems early in the mission, the docking was successful on the first attempt, though the LM's Abort Guidance System, used for navigation, failed just before the two craft docked. After crew, equipment, and lunar samples were transferred to Kitty Hawk, the ascent stage was jettisoned, and impacted the Moon,[109][110] setting off waves registered by the seismometers from Apollo 12 and 14.[111]

A trans-earth injection burn took place on February 6 at 8:39:04 pm (February 7 at 01:39:04 UTC) taking 350.8 seconds, during Kitty Hawk's 34th lunar revolution.[42][112] During the trans-earth coast, two tests of the oxygen system were performed, one to ensure the system would operate properly with low densities of oxygen in the tanks, the second to operate the system at a high flow rate, as would be necessary for the in-flight EVAs scheduled for Apollo 15 and later. Additionally, a navigation exercise was done to simulate a return to Earth following a loss of communications. All were successful.[113] During his rest periods on the voyage, Mitchell conducted ESP experiments without NASA's knowledge or sanction, attempting by prearrangement to send images of cards he had brought with him to four people on Earth. He stated after the mission that two of the four had gotten 51 out of 200 correct (the others were less successful), whereas random chance would have dictated 40.[114][115] On the final evening in space, the crew conducted a press conference, with the questions submitted to NASA in advance and read to the astronauts by the CAPCOM.[116]

The command module Kitty Hawk splashed down in the South Pacific Ocean on February 9, 1971, at 21:05 [UTC], approximately 900 miles (1,400 km) south of American Samoa. After recovery by the ship USS New Orleans,[117] the crew was flown to Pago Pago International Airport in Tafuna, then to Honolulu, then to Ellington Air Force Base near Houston in a plane containing a Mobile Quarantine Facility trailer before they continued their quarantine in the Lunar Receiving Laboratory.[118] They remained there until their release from quarantine on February 27, 1971.[119] The Apollo 14 astronauts were the last lunar explorers to be quarantined on their return from the Moon. They were the only Apollo crew to be quarantined both before and after the flight.[120]

Roosa, who worked in forestry in his youth, took several hundred tree seeds on the flight. These were germinated after the return to Earth, and were widely distributed around the world as commemorative Moon trees.[121] Some seedlings were given to state forestry associations in 1975 and 1976 to mark the United States Bicentennial.[122]

Mission insignia

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Apollo 14 space-flown silver Robbins medallion

The mission insignia is an oval depicting the Earth and the Moon, and an astronaut pin drawn with a comet trail.[123] The pin is leaving Earth and is approaching the Moon.[124] A gold band around the edge includes the mission and astronaut names. The designer was Jean Beaulieu,[123] who based it on a sketch by Shepard, who had been head of the Astronaut Office and meant the pin to symbolize that through him, the entire corps was in spirit flying to the Moon.[32]

The backup crew spoofed the patch with its own version, with revised artwork showing a Wile E. Coyote cartoon character depicted as gray-bearded (for Shepard, who was 47 at the time of the mission and the oldest man on the Moon), pot-bellied (for Mitchell, who had a pudgy appearance) and red-furred (for Roosa's red hair), still on the way to the Moon, while Road Runner (for the backup crew) is already on the Moon, holding a U.S. flag and a flag labelled "1st Team".[125] The flight name is replaced by "BEEP BEEP" and the backup crew's names are given. Several of these patches were hidden by the backup crew and found during the flight by the crew in notebooks and storage lockers in both the CSM Kitty Hawk and the LM Antares, and one patch was stored in the MET lunar handcart.[82] One patch, attached to Shepard's PLSS, was worn on the lunar surface, and, mounted on a plaque, was presented by him to Cernan after the mission.[125]

Spacecraft locations

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The command module Kitty Hawk at the Kennedy Space Center in Florida

The Apollo 14 command module Kitty Hawk is on display at the Apollo/Saturn V Center at the Kennedy Space Center Visitor Complex after being on display at the United States Astronaut Hall of Fame near Titusville, Florida, for several years.[126] At the time of its transfer of ownership from NASA to the Smithsonian in July 1977, it was on display at the facilities of North American Rockwell (the company that had constructed it) in Downey, California.[47] The SM reentered Earth's atmosphere and was destroyed, though there was no tracking or sightings of it.[127]

The S-IVB booster impacted the Moon on February 4 at 8°10′52″S 26°01′50″W / 8.181°S 26.0305°W / -8.181; -26.0305 (Apollo 14 S-IVB).[128] The ascent stage of lunar module Antares impacted the Moon on February 7, 1971, at 00:45:25.7 UT (February 6, 7:45 pm EST), at 3°25′S 19°40′W / 3.42°S 19.67°W / -3.42; -19.67 (Apollo 14 LM ascent stage).[128] Antares' descent stage and the mission's other equipment remain at Fra Mauro at 3°39′S 17°28′W / 3.65°S 17.47°W / -3.65; -17.47 (Apollo 14 LM descent stage).[4]

Photographs taken in 2009 by the Lunar Reconnaissance Orbiter were released on July 17, and the Fra Mauro equipment was the most visible Apollo hardware at that time, owing to particularly good lighting conditions. In 2011, the LRO returned to the landing site at a lower altitude to take higher resolution photographs.[129]

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See also

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References

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Bibliography

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Revisions and contributorsEdit on WikipediaRead on Wikipedia
from Grokipedia
Apollo 14 was the eighth crewed Apollo mission and the third to achieve a lunar landing, launched by NASA on January 31, 1971, from Kennedy Space Center in Florida aboard a Saturn V rocket. The mission's primary objectives included exploring the Fra Mauro formation (originally targeted by the aborted Apollo 13 mission) in the lunar highlands, deploying the Apollo Lunar Surface Experiments Package (ALSEP) to conduct long-term scientific measurements, and collecting geological samples to study the Moon's early history. Commander Alan B. Shepard Jr. and Lunar Module Pilot Edgar D. Mitchell descended to the surface in the Lunar Module Antares on February 5, landing at coordinates 3°40'27"S, 17°27'58"W, while Command Module Pilot Stuart A. Roosa orbited above in Kitty Hawk to perform scientific observations and photography. The crew consisted of experienced astronauts: Shepard, America's first man in space on Mercury-Redstone 3 in 1961 and the only Mercury astronaut to return to flight, served as mission commander; Roosa, a rookie , managed the command module; and Mitchell, also on his first , piloted the . Over two extravehicular activities (EVAs) lasting a total of 9 hours and 24 minutes—the longest to date—Shepard and Mitchell traversed approximately 3.45 kilometers using the Modularized Equipment Transporter (MET), a hand-pulled cart for tools and samples, and deployed the ALSEP instruments including a , , and for laser ranging. They collected 42.9 kilograms of lunar rocks and soil, including breccias from the highlands that provided insights into the Moon's bombardment history. Notable achievements included the most precise lunar landing up to that point, approximately 87 feet from the target, and overcoming challenges like a docking issue resolved after six attempts following the abort. Shepard famously hit two golf balls on the lunar surface with a makeshift club during the second EVA, a lighthearted moment broadcast worldwide that highlighted human ingenuity in low gravity. Roosa's orbital activities included capturing high-resolution images and stellar , while the mission's success restored confidence in the after the near-disaster of . The spacecraft splashed down in the on February 9, 1971, precisely nine days and two minutes after launch, approximately 1,400 kilometers south of —1.02 nautical miles from the recovery ship target.

Background and Objectives

Mission Overview

Apollo 14 was the third successful lunar landing mission in NASA's , launched on January 31, 1971, at 21:03 UTC from Launch Complex 39A at the in . The crew consisted of Commander Alan B. Shepard Jr., who commanded the mission and walked on the ; Pilot Edgar D. Mitchell, who also performed lunar surface activities; and Command Module Pilot Stuart A. Roosa, who remained in . The mission lasted 9 days and 2 minutes, concluding with splashdown in the on February 9, 1971. It targeted the Fra Mauro formation in the lunar highlands as the landing site, selected for its geological significance in accessing ejecta from the ancient Imbrium basin impact. The primary objectives of Apollo 14 included conducting the third crewed lunar landing, exploring the Fra Mauro region to collect rock and soil samples that would provide insights into the Moon's early history, and deploying the Apollo Lunar Surface Experiments Package (ALSEP) to conduct long-term scientific measurements. This mission served as a critical follow-up to the aborted Apollo 13 landing in April 1970, which had highlighted risks in the program and prompted extensive safety modifications; the overall Apollo program was estimated to cost around $25 billion, with ongoing flights demonstrating restored confidence in the Saturn V rocket and spacecraft systems. Key achievements of Apollo 14 previewed advancements in lunar exploration, including two extravehicular activities (EVAs) by Shepard and Mitchell totaling 9 hours and 24 minutes on the surface, during which they traversed up to 1.4 kilometers from the using the newly introduced Modular Equipment Transporter (MET), a hand-pulled cart for carrying tools and samples. The collected approximately 42 kilograms of lunar material, contributing to geological studies of the highlands, and successfully deployed the ALSEP station, which operated until shut down in 1977. These efforts marked a step toward more extended surface operations in subsequent missions.

Scientific Goals

The primary scientific goal of Apollo 14 was to perform selenological inspection, survey, and sampling of materials in the Fra Mauro region, which consists predominantly of from the Imbrium impact basin, to elucidate lunar and the processes involved in basin formation. This objective focused on collecting rock and soil samples that would allow scientists to analyze the composition, stratigraphy, and age of the ejecta blanket, providing insights into the cataclysmic events that shaped the Moon's crust approximately 3.9 billion years ago. The Fra Mauro site was selected specifically for its representation of pre-mare highland terrain, enabling direct study of ancient impact dynamics without the overlay of younger basaltic lavas. A key component of the mission's scientific objectives involved the deployment and activation of the Apollo Lunar Surface Experiments Package (ALSEP), a suite of instruments designed for long-term monitoring of the lunar environment. The ALSEP for Apollo 14 included the Active Seismic Experiment (ASE) to profile the structure, the Passive Seismic Experiment (PSE) to detect moonquakes, the Charged Particle Lunar Environment Experiment (CPLEE) to measure particle fluxes, the Suprathermal Ion Detector Experiment (SIDE) and Cold Cathode Ion Gauge Experiment (CCIG) to assess the and populations, the Lunar Detector Experiment to monitor electrostatic dust movement, and the (LRRR) for precise distance measurements. These instruments aimed to gather data on geophysical properties, solar interactions, and surface processes to calibrate models of lunar evolution. Traverse planning emphasized geological exploration along a approximately 3-km path from the landing site to the rim of , a 340-meter-diameter secondary that exposes subsurface layers of Imbrium . Astronauts were tasked with mapping surface features, documenting through photography and core sampling, and selectively collecting rocks to represent the vertical sequence of highland materials. This structured traverse, conducted during two extravehicular activities, sought to provide a cross-section of the and , aiding in the reconstruction of impact excavation and deposition mechanisms. Overall, these goals contributed to broader understandings of lunar by enabling seismic profiling of the via the ASE's thumper and array, which targeted shallow velocity structures, and by facilitating the collection of solar wind-implanted materials through surface samples for isotopic of ancient solar activity. The mission's emphasis on Fra Mauro's unique helped refine evolutionary models of the Moon's bombardment history and interior differentiation.

Crew and Personnel

Prime and Backup Crew

The prime crew for Apollo 14 was Commander Alan B. Shepard Jr., Command Module Pilot Stuart A. Roosa, and Lunar Module Pilot Edgar D. Mitchell. Alan B. Shepard Jr., aged 47, served as the mission commander. A U.S. Navy , he had become the first American in space aboard in 1961 but was grounded from 1963 to 1969 due to , an inner ear disorder affecting balance. Cleared for flight in 1969, Shepard's extensive experience in early programs positioned him ideally to lead the third lunar landing mission. Edgar D. Mitchell, aged 40, acted as lunar module pilot. Selected as an in 1966, he was a U.S. Navy aviator and who earned a PhD in and from MIT in 1964. Mitchell's advanced academic background in science and engineering supported the mission's emphasis on lunar surface exploration and experimentation. Following the mission, he developed a keen interest in phenomena and studies, founding the Institute of Noetic Sciences in 1973 to investigate such topics. Stuart A. Roosa, aged 37, piloted the command module. An test pilot selected in NASA's fifth astronaut group in 1966, Roosa brought prior experience as a U.S. Forest Service , fighting wildfires in remote areas during the 1950s. This forestry background directly influenced his role in a joint NASA-U.S. Forest Service experiment, where he carried hundreds of tree seeds in to study space radiation effects, later germinating them into "." His proven skills in high-performance aircraft handling were critical for the command module's solo operations during the lunar landing. The backup crew included Commander Eugene A. Cernan, Command Module Pilot Ronald E. Evans, and Lunar Module Pilot Joe H. Engle. Cernan, aged 36, was an pilot and veteran of and , providing seasoned leadership support. Evans, aged 37, was a aviator selected in 1966 with expertise in and carrier-based operations. Engle, aged 38, was an test pilot renowned for flying the X-15 rocket plane to the edge of space three times, qualifying him for contingencies. Crew selection emphasized complementary expertise: Shepard's command experience ensured mission oversight, Mitchell's scientific credentials enhanced geological and experimental objectives, and Roosa's orbital piloting proficiency maintained command module stability. The backups mirrored this balance, with Cernan's prior lunar rehearsal on , Evans's navigation skills, and Engle's hypersonic test flight background for potential surface operations. Overall dynamics highlighted Shepard's triumphant return after medical challenges, fostering a motivated team, while Mitchell's later pursuits in anomalous phenomena and Roosa's environmental ties added unique post-mission legacies.

Key Mission Control Roles

The Mission Control Center for Apollo 14 was located at the Manned Spacecraft Center in Houston, Texas (now ), where specialized teams of flight controllers provided continuous oversight through rotating shifts to ensure 24/7 mission support. These teams operated from the Mission Operations Control Room, coordinating all aspects of the flight from launch through . Flight Directors led each shift, holding ultimate authority for real-time decisions under established mission rules. directed the White Team during critical phases, including launch and aspects of the lunar landing preparations, drawing on his experience from prior Apollo missions to guide the team through high-stakes operations. led the Black Team for several key intervals. Gerry Griffin led the Gold Team during the lunar module descent, where his leadership was instrumental in resolving a in the abort switch that briefly illuminated during powered descent. The ground team under Griffin, working with from the crew, determined the issue stemmed from floating in the switch mechanism and recommended proceeding with the landing, averting an unnecessary abort and enabling successful touchdown at Fra Mauro. Essential support roles included the Capsule Communicator (CAPCOM), the only flight controller authorized to speak directly to the astronauts; Fred Haise, the Apollo 13 lunar module pilot, served as CAPCOM during lunar surface operations, leveraging his recent mission training to provide precise guidance on traverses and experiments. The Flight Dynamics Officer (FDO) tracked orbital trajectories and maneuver performance, while the Guidance Officer (GUIDO) monitored navigation and attitude control systems. The Electrical, Environmental, and Consumables Manager (EECOM) oversaw spacecraft power, life support, and communications integrity. These positions collaborated closely during translunar injection and subsequent midcourse corrections, executing two precise burns—at approximately 30.5 and 77 hours mission elapsed time—to align the trajectory for lunar orbit insertion.

Preparation and Training

Crew Selection and Assignment

The selection and assignment of the Apollo 14 crew followed NASA's standard rotation policy for lunar landing missions, where backup crews from one mission typically advanced to prime roles for a subsequent flight approximately 18 months later. This process was initiated after the assignment of the crew in early 1969, with the Apollo 14 prime and backup teams formally announced by on August 6, 1969. The prime crew included Commander Alan B. Shepard Jr., a U.S. Navy captain and the first American in space on in 1961; Command Module Pilot Stuart A. Roosa, a U.S. Air Force major; and Lunar Module Pilot Edgar D. Mitchell, a U.S. Navy commander. All three possessed extensive experience, meeting NASA's qualifications for piloting complex spacecraft and conducting extravehicular activities. Shepard's assignment as was a notable exception to NASA's typical criteria regarding age and recent flight experience, as he was 47 years old at the time of launch—the oldest to fly on an Apollo mission. Grounded since 1964 due to , an inner-ear disorder causing vertigo and balance issues, Shepard underwent experimental surgery in that restored his flight eligibility, allowing his return to . This medical clearance, approved by NASA management including Administrator , enabled Shepard to lead Apollo 14 despite not having flown since his Mercury mission nearly a decade earlier. The backup crew for Apollo 14 consisted of Commander Eugene A. Cernan, a U.S. captain who had flown on ; Command Module Pilot Ronald E. Evans, a U.S. lieutenant commander; and Lunar Module Pilot Joe H. Engle, a U.S. Air Force major with X-15 experience. In line with NASA's rotation system, this team progressed to the prime crew for , the program's final lunar landing mission in December 1972, though Engle was later replaced by geologist Harrison H. Schmitt to prioritize scientific expertise on the surface. Reflecting the composition of NASA's astronaut corps in the late 1960s, the Apollo 14 crew was entirely male and drawn from military backgrounds, with no civilian representation—a pattern that persisted until Schmitt's inclusion on Apollo 17. This selection emphasized test pilot skills and operational reliability over broader diversity considerations at the time.

Training Exercises and Simulations

The Apollo 14 crew participated in intensive geological field training to develop skills in rock identification, sampling techniques, and terrain navigation relevant to the Fra Mauro formation's volcanic and impact features. These exercises took place in analog sites across the United States and abroad, emphasizing hands-on observation under conditions mimicking lunar geology. Led by NASA geologists including Harrison Schmitt, who provided instruction on lunar feature recognition and sample collection for multiple Apollo missions, the training built the crew's ability to document and collect scientifically valuable materials during extravehicular activities. Key field trips for the Apollo 14 prime and backup crews included sessions in Hawaii's volcanic landscapes, such as the Kapoho area, where participants practiced traversing rugged lava fields and identifying basaltic rocks similar to those expected on the Moon. In Arizona, exercises near Flagstaff focused on flyover geology and surface traverses to simulate orbital and landing site observations, with Command Module Pilot Stuart Roosa and backup pilot Ron Evans participating in aerial mapping drills. Additional training occurred in New Mexico at sites like Kilbourne Hole, an impact crater analog, allowing the crew to study ejecta patterns and breccias while honing sampling protocols. Although earlier Apollo groups had trained in Iceland's volcanic terrain in 1965 and 1967, the Apollo 14 regimen prioritized U.S.-based sites for more targeted Fra Mauro simulations following the mission's site change from Littrow. EVA simulations formed a core component of the crew's preparation, utilizing facilities to replicate low-gravity mobility in pressure suits. At NASA's Neutral Buoyancy Simulator in , astronauts practiced deploying and maneuvering the Modularized Equipment Transporter (MET), a wheeled cart for carrying tools and samples, as well as core tube sampling and contingency procedures in a simulated lunar environment. These underwater sessions, conducted over dozens of hours, addressed suited dexterity challenges unique to the Fra Mauro's hilly terrain, including balance during uphill traverses and tool handling with reduced weight. Integrated mission rehearsals integrated these skills into full-scale simulations at Cape Kennedy (now ) and the Manned Spacecraft Center (now ) in . These multi-day exercises replicated the entire mission timeline, from launch to lunar surface operations, incorporating abort scenarios such as engine failures during descent or ascent. Particular emphasis was placed on the planned 3-kilometer traverse to Cone Crater, where crews practiced timeline management, communication with Mission Control, and decision-making under time constraints using mockups of the and surface tools. Over 1,000 hours of such simulations ensured procedural familiarity and team coordination. Unique aspects of the training reflected individual crew roles and personal initiatives. Commander , drawing from his aviation background, informally practiced golf swings with a modified six-iron attached to a lunar sampling handle during simulator sessions, conceptualizing a lighthearted demonstration of lunar that he later executed on the . Lunar Module Pilot , leveraging his aeronautical engineering expertise, concentrated on navigation drills using stereoscopic maps and alignments to prepare for the undulating Fra Mauro , which posed visibility challenges during the Cone Crater hike. Command Module Pilot completed centrifuge runs at the Naval Aviation Medical Acceleration Laboratory to acclimate to reentry g-forces up to 7 Gs, simulating the command module's atmospheric deceleration while maintaining control inputs.

Hardware and Equipment

Command and Service Module

The Apollo 14 Command and Service Module (CSM), designated as CSM-110 and named Kitty Hawk, utilized the Block II configuration developed by for crewed lunar missions. This design featured a conical Command Module (CM) mated to a cylindrical Service Module (SM), with an overall height of approximately 11 meters and a base diameter of 3.9 meters. The fully fueled mass at launch was about 30,000 kilograms, enabling the spacecraft to support the crew during translunar transit, , and return to Earth. The CM included three hatches—two side hatches and one forward docking hatch—each with dimensions of approximately 29 inches (74 cm) high by 34 inches (86 cm) wide, providing an area of roughly 7 square feet (0.65 square meters) to facilitate crew entry, , and docking with the Lunar Module. Following the Apollo 13 incident, implemented several modifications to the Apollo 14 CSM to enhance reliability, particularly in propulsion and power systems. The (RCS) thrusters were improved with additional propellant tanks and redundant wiring to prevent potential failures in attitude control during critical maneuvers. The SM's Scientific Instrument Module (SIM) bay was also enhanced to better accommodate orbital science payloads, including improved mounting for sensors to withstand launch vibrations. These changes, along with redesigned oxygen tanks featuring better temperature sensors and circuit protection, addressed vulnerabilities exposed in the prior mission without altering the core Block II architecture. The Service Module housed essential propulsion and support systems for the CSM. Its primary Service Propulsion System (SPS) engine delivered 20,500 pounds-force (91 kN) of using an AJ10-137 hypergolic engine, fueled by and nitrogen tetroxide, to perform major trajectory corrections like insertion and trans-Earth injection. Power was supplied by three hydrogen-oxygen fuel cells, generating up to 2.3 kilowatts continuously, while the RCS consisted of 16 (four quads) providing 440 newtons of each for precise orientation. These systems operated nominally throughout the mission, supporting the CSM's role in orbital operations. The Apollo 14 SM's SIM bay, located in the forward section, carried key scientific instruments for lunar orbital observations. These included the Gamma-ray Spectrometer, which mapped and other elements on the lunar surface; the experiment, which analyzed elemental composition; the Solar Wind Composition experiment, which used a foil collector to capture particles; and the Particles and Fields Subsatellite, released to study the Moon's and particles. Film cassettes from these instruments were retrieved post-mission for analysis, yielding data on lunar geology and the tenuous . Command Module Pilot Stuart A. Roosa managed solo operations in while his crewmates explored the surface, focusing on visual observations and to document geological features like craters and maria. He exposed multiple film cassettes using handheld cameras for high-resolution synoptic views, complementing SIM bay data, and conducted bare-eye assessments of the Moon's . No significant issues arose during these activities, with the CSM systems performing reliably to ensure a safe rendezvous and return.

Lunar Module

The Apollo 14 , designated LM-8 and named , served as the lander for the mission's exploration of the Fra Mauro formation. Built by Aerospace Corporation, it followed the standard Block II configuration for Apollo H-type missions, with the descent stage housing propellant tanks, , and scientific instrument bays, while the ascent stage contained the crew cabin, life support systems, and propulsion for lunar liftoff. The overall structure stood approximately 7.04 meters tall from the base of the descent stage to the top of the ascent stage (excluding extended landing probes), with a maximum of 4.2 meters, and had a fueled of about 15,264 kilograms, including crew, , and roughly 11,010 kilograms of propellants. This design enabled a maximum descent of around 2.5 meters per second at , supported by the landing radar's velocity measurements during powered descent. Key modifications to addressed lessons from prior missions, enhancing reliability for the Fra Mauro landing site. Following Apollo 12's docking experiences, the probe-and-drogue mechanism was refined with improved latch mechanisms and capture rings to reduce the risk of incomplete engagement during command module extraction from the S-IVB adapter. Post-Apollo 13's service module , the ascent stage guidance and navigation system (including the and abort electronics) was upgraded with redundant signal filtering to prevent false abort triggers from vibration or electrical noise, ensuring stable control during ascent. These changes were part of broader post-Apollo 13 safety enhancements, including additional battery capacity and improved wiring insulation in the LM electrical systems. The LM's propulsion systems were critical for lunar operations, with the descent propulsion system (DPS) hypergolic engine delivering a maximum of 45 kilonewtons, throttleable from 10% to 100% for precise control during the 12-minute powered descent burn. Four ascent propulsion system (APS) ullage thrusters, each producing 0.44 kilonewtons, settled propellants and provided initial attitude stabilization before main engine ignition. The pressurized crew cabin offered 4.35 cubic meters of habitable volume, sufficient for two astronauts during the 33-hour surface stay, and featured a 0.81-by-0.81-meter square EVA hatch that facilitated extravehicular activities with minimal repressurization time. During the actual lunar landing on February 5, 1971, encountered a significant challenge when the descent engine shut down twice prematurely, triggered by an erroneous abort signal from the commander's abort stage switch being inadvertently bumped amid the vibrations of descent. This glitch, stemming from unfiltered switch bounce in the guidance computer interface, halted the DPS burn at about 3,000 meters and again shortly after restart, threatening an abort. Commander and Lunar Module Pilot resolved it through manual override, using a felt-tip pen to secure the switch in the "off" position and bypassing the automatic abort logic, allowing the engine to reignite and complete the 53 meters (174 feet) from the target site with a touchdown velocity of 0.52 m/s (1.7 ft/s) horizontal and 0.94 m/s (3.1 ft/s) vertical.

Saturn V Launch Vehicle

The Saturn V launch vehicle designated SA-509 carried the Apollo 14 mission into space. Standing 110.6 meters tall, it had a liftoff mass of approximately 2,950,867 kilograms and consisted of three main stages: the first stage, second stage, and third stage, along with the instrument unit for guidance. The stage measured 33 meters in length and 10 meters in diameter, while the overall stack integrated the Command and Service Module and as the payload atop the . The first stage was powered by five liquid-fueled engines, each delivering about 6.77 meganewtons of thrust at using kerosene and . The second stage employed five engines, each producing approximately 0.89 meganewtons at (1.02 meganewtons in vacuum) with and propellants. The third stage utilized a single J-2 engine of the same configuration. These engines enabled the to achieve the necessary velocity for parking orbit and subsequent translunar injection. In performance, SA-509 delivered a translunar payload of about 48,600 kilograms to a trajectory targeted for a free-return path with a pericynthion altitude of 3,253 kilometers at the Moon. The S-IVB stage's translunar injection burn lasted roughly 6 minutes, boosting the stack from parking orbit to escape velocity. The launch window opened at 15:23 Eastern Standard Time on January 31, 1971, with liftoff occurring at 16:03:02 EST from Pad 39A at Kennedy Space Center. Following the Apollo 13 incident, SA-509 underwent extensive safety inspections and verification tests across its stages and systems to ensure reliability, including checks on propulsion and separation mechanisms. An improved design for the S-IC/S-II interstage facilitated smoother separation during ascent. The payload integration briefly referenced the CSM and LM stacked above the S-IVB for the full mission configuration.

Surface Equipment and Tools

The Apollo Lunar Surface Experiments Package (ALSEP) consisted of several scientific instruments designed for long-term monitoring of the lunar environment, including a passive seismic experiment, active seismic device, suprathermal ion detector, charged particle lunar environment experiment, and cold cathode ion gage. The package, weighing 83 kg, was deployed approximately 180 m west of the during the first (EVA). Powered by a (RTG) that produced 73 W of electrical power, the ALSEP featured a with omnidirectional and high-gain antennas for transmitting data back to stations. Deployment involved leveling the site and aligning the instruments, enabling continuous geophysical observations for over a year post-mission. To support extended traverses, Apollo 14 introduced the Modular Equipment Transporter (MET), a lightweight, hand-pulled cart constructed from tubular aluminum . Empty, the MET weighed 11.3 kg and measured about 91 cm in length, 76 cm in width, and 30 cm in height when operational, with a stowage envelope of 71 cm × 91 cm × 20 cm for transport in the . Capable of carrying up to 63.5 kg of payload—including tools, sample bags, cameras, and contingency items—it featured wire-mesh wire wheels for traction on the and foldable legs for stability when stationary. Astronauts Shepard and Mitchell pulled the MET during their second EVA, covering nearly 2 km to Cone Crater and back, marking its debut as a mobility aid for lunar exploration. A suite of portable tools enabled geological sampling and documentation on the surface. Core tubes, with a 2-cm diameter, allowed collection of subsurface samples; individual tubes measured 91 cm in length, and up to three could be connected for depths reaching 3 m using a drive tube extension and hammer. Tongs, adjustable for gripping rocks from 2.5 to 15 cm in size, facilitated non-contaminating sample handling, while the —a 38-cm staff with color chips, scales, and a bubble level—provided reference for shadow angles and in photographs. Hasselblad electric cameras, modified 500EL models with 80-mm or 250-mm lenses, captured over 1,000 high-resolution images in color and black-and-white film. The Apollo Lunar Ranging (ALRR), a 0.46 m × 0.46 m panel of 100 corner-cube prisms weighing 2.6 kg, was precisely leveled and deployed 40 m from the to reflect Earth-based beams for distance measurements. Additionally, a 3.7 m × 1.1 m U.S. was erected near the descent , and a stainless-steel plaque inscribed "We came in peace for all mankind," signed by the crew and President Nixon, was mounted on the . Commander Shepard also improvised a by attaching a club head to the of a contingency lunar sample tool, using it to hit two golf balls during EVA closeout.

Launch and Translunar Injection

Liftoff and Early Orbit

The countdown for Apollo 14 commenced at T-28 hours on January 30, 1971, with a planned built-in hold of nine hours and 23 minutes at T-8 hours and 5 minutes to allow for crew rest and systems preparations. A brief 40-minute hold was inserted near the end of the countdown due to showers and cloud cover over the , ensuring safe weather conditions before proceeding. Liftoff occurred nominally at 4:03 p.m. EST on January 31, 1971, from Launch Complex 39A, aboard the rocket designated SA-509. The first stage (S-IC) burn proceeded as planned for 168 seconds, accelerating the vehicle to approximately 2.7 km/s and an altitude of about 68 km before separation. Subsequent staging events, including S-IC/S-II separation and S-II ignition, were nominal, with the vehicle performing a roll program shortly after liftoff—consisting of programmed yaw and roll maneuvers—to establish the proper launch of 72.1 degrees for downrange tracking and orbital insertion. The (IMU) provided guidance throughout powered flight, maintaining alignment with the pre-launch platform orientation without significant deviations. Apollo 14 achieved an Earth parking orbit of approximately 190 by 197 km after cutoff. The crew completed two orbits over about 89 minutes, conducting thorough systems checks on the command and service module, , and propulsion systems, confirming no major anomalies in contrast to the service module damage experienced later in Apollo 13.

Trajectory to the Moon

The (TLI) burn commenced with the ignition of the stage's J-2 engine at 2 hours, 28 minutes, and 32 seconds ground elapsed time (GET) following launch, lasting 350.8 seconds and accelerating the to a of approximately 10.8 km/s. This maneuver transitioned the Apollo 14 stack from an initial with a perigee of about 190 km to a intersecting the Moon's orbit roughly 76 hours later. The burn's precision, informed by ground tracking data, minimized the need for subsequent adjustments and ensured efficient propellant usage. Shortly after TLI, at approximately 3 hours GET, the crew executed transposition, docking, and extraction (TDE) maneuvers. Command Module Pilot Stuart A. Roosa maneuvered the Command and Service Module (CSM) independently using its Reaction Control System (RCS) thrusters to separate from the S-IVB and approach the Lunar Module (LM). However, docking proved challenging due to misalignment of the probe capture latches, requiring six attempts over 1 hour and 42 minutes before achieving a successful hard dock at 4 hours, 56 minutes GET through manual thruster adjustments to hold the vehicles together. The LM was then extracted from the S-IVB adapter, with systems checks confirming nominal performance of both spacecraft. The separation from the S-IVB occurred at 5 hours, 47 minutes GET, sending the spent stage on a trajectory to lunar impact. Over the subsequent three-day coast, three midcourse corrections (MCCs) were planned to fine-tune the trajectory, utilizing the CSM's RCS thrusters for small velocity changes. Due to the TLI burn's accuracy, the first correction (MCC-1), scheduled around 11 hours GET, was omitted. MCC-2 took place at 30 hours, 36 minutes GET with a firing duration of 10.1 seconds (delta-V of 21.7 m/s), followed by MCC-3 at 76 hours, 58 minutes GET lasting 0.65 seconds (delta-V of 1.1 m/s); these maneuvers provided a total delta-V of approximately 23 m/s, aligning the spacecraft for insertion without significant deviations. Navigation relied on continuous ground-based radiometric tracking from the Manned Space Flight Network stations worldwide, supplemented by onboard optical observations. The crew used the CSM's and scanning telescope for periodic sightings to verify attitude and independently assess parameters, confirming alignment with predictions and detecting no major anomalies. Throughout the translunar phase, the crew conducted routine systems monitoring, televised views of and deep space to ground control, and lightweight exercise to maintain physical condition, interspersed with scheduled sleep periods.

Lunar Operations

Orbit Insertion and Descent

Apollo 14 reached the Moon after approximately 82 hours and 36 minutes of ground elapsed time (GET), when the Command and Service Module (CSM) Kitty Hawk performed the Lunar Orbit Insertion-1 (LOI-1) burn using its Service Propulsion System (SPS) engine. The retrograde burn ignited behind the , out of direct communication with Earth, and lasted 6 minutes and 7 seconds, imparting a delta-V of 921.2 m/s to capture the spacecraft into an initial elliptical of 57 by 170 nautical miles (105 by 315 km). This maneuver placed the stacked CSM and Lunar Module (LM) Antares into a stable inclined at approximately 14 degrees to the lunar equator, optimized for the mission's landing site in the Fra Mauro highlands. Following two orbits to verify systems and conduct preliminary observations, the crew prepared for further orbital adjustments. At about 87 hours GET, the CSM performed the Descent Orbit Insertion (DOI) burn, another SPS firing lasting 20.8 seconds and delivering a delta-V of approximately 62.9 m/s, which lowered the orbit's pericynthion to 9.1 nautical miles (16.9 km) while maintaining an apocynthion of about 58 nautical miles (107 km). This adjustment, unique to Apollo 14 as the first mission where the CSM rather than the LM handled the DOI, conserved LM propellant for the descent phase and positioned the spacecraft for landing preparations. and Lunar Module Pilot then transferred to the LM during the subsequent orbits, leaving Command Module Pilot in the CSM. Undocking occurred at 104 hours and 26 minutes GET, during the fourth full , after Shepard and Mitchell completed LM activation and systems checks. A planned docking rehearsal was canceled due to ongoing concerns with the CSM's docking probe mechanism, which had malfunctioned repeatedly during translunar flight and required extensive . The separation was executed smoothly with a short RCS burn by the CSM, placing the LM on a for powered descent initiation at pericynthion. The crew reported clear visual confirmation of separation, with Antares descending toward the lunar surface as Kitty Hawk adjusted to a higher for Roosa's solo operations. As Antares began powered descent at approximately 108 hours GET, using the LM Descent Propulsion System (DPS) engine for a 12-minute burn, the crew encountered a critical anomaly: a false abort signal illuminated on the control panel about 8 minutes into the burn, at an altitude of approximately 11,100 meters (36,500 feet). Caused by a loose particle intermittently shorting the abort switch circuitry, the signal triggered alarms and threatened an automatic ascent stage separation, potentially aborting the landing. To resolve it, the ground team had devised a software workaround using the to inhibit the abort mode, which the crew executed along with manual overrides by cycling the PROCEED switch and tapping the panel to dislodge the fault, resolving the issue after about 10 minutes of heightened tension without interrupting the descent. Earlier, the landing radar had failed to acquire a signal automatically; the crew reset it by cycling the , achieving lock-on at 22,486 feet (6,856 meters) altitude, providing essential velocity and range data for the final approach. These interventions ensured the LM continued safely toward touchdown in the Fra Mauro region.

Lunar Landing and First EVA

The Lunar Module Antares touched down in the Fra Mauro highlands at 4:18 a.m. EST on February 5, 1971, approximately 53 meters (55 feet north, 165 feet east) from the targeted site, with a final descent rate of approximately 0.9 m/s (3 ft/s). Commander reported the successful landing, stating, "Houston, Antares is on the surface." The landing occurred at ground elapsed time (GET) 108:15, following a powered descent that included manual adjustments to avoid boulders and ensure a safe touchdown on uneven terrain. After , the performed systems checks and a brief rest period before beginning cabin depressurization approximately 5 hours later, at approximately 113 hours GET. Shepard egressed first at 113 hours 39 minutes GET, stepping onto the lunar surface and marking his return to after a decade, followed shortly by Pilot at 113 hours 45 minutes GET. The astronauts faced initial challenges with the porch probe switch, which delayed hatch opening by about 15 minutes, but they resolved it without aborting the procedure. The first extravehicular activity (EVA) lasted 4 hours 48 minutes, from 113:39 to 118:27 GET, focusing on immediate site setup and short-range exploration. Shepard and Mitchell deployed the Apollo Lunar Surface Experiments Package (ALSEP) approximately 185 meters west-northwest of the Lunar Module, positioning instruments including the Passive Seismic Experiment and Charged Particle Lunar Environment Experiment to study lunar seismicity and solar wind interactions. They assembled the Modular Equipment Transporter (MET), a hand-pulled cart for carrying tools and samples, using equipment stored in the Lunar Module's descent stage. A brief traverse of about 50 meters took them to the rim of Flag Crater, a small 3-meter-wide depression, where they collected contingency samples and documented the regolith with photographs. During this EVA, they gathered roughly 10 kg of lunar material, including soil and rock fragments, while live television coverage beamed the activities to Earth, capturing Shepard's steps and the deployment process. Several contingencies arose during the landing and EVA, including dust kicked up by the descent engine that temporarily obscured the horizon and complicated final , though it settled quickly without impacting visibility long-term. Minor mobility restrictions, particularly in the gloves and shoulders, were noted due to the pressurized suits' stiffness in the low- environment, but they did not hinder core tasks. The MET assembly proceeded smoothly on the surface despite the awkward positioning required in 1/6th gravity, aided by simple hand tools like the adjustable sample bag holder.

Second EVA and Traverse

The second (EVA) commenced on February 6, 1971, at 4:15 a.m. EST, equivalent to Ground Elapsed Time (GET) of 131 hours 8 minutes, and extended for 4 hours and 35 minutes. Pilot was the first to egress the Antares, followed by Commander . This EVA focused on an ambitious geological traverse aimed at reaching the rim of Cone Crater to collect samples from diverse terrains within the Fra Mauro formation. The traverse covered approximately 1.5 kilometers each way from the landing site to the crater rim, utilizing the Modularized Equipment Transporter (MET), a hand-pulled cart designed to carry tools and samples. Cone Crater, an impact feature roughly 300 meters in diameter, lay at an elevation gain of about 120 meters above the Lunar Module site, with the route marked by way stations using colored flags for navigation. The path ascended gradually over undulating terrain, incorporating stops at six designated stations where the astronauts documented and sampled lunar breccias, soil fines, and rocks to analyze the ejecta blanket and subsurface . Activities included extensive photography to record geological context, as well as core drilling that achieved a depth of 2.3 meters at one station, providing a vertical profile of the . Several challenges marked the traverse, including the steep uphill that strained the astronauts' mobility in their pressurized suits and contributed to physical after more than nine hours of total surface time. The MET experienced wheel malfunctions, with debris causing intermittent binding and requiring manual interventions to maintain progress. proved particularly difficult due to the monotonous, -dotted landscape, leading to disorientation; the missed the crater rim by approximately 30 meters before recognizing their position from topographic cues and aligning with pre-planned azimuths. Near the EVA's conclusion, as they returned to the Lunar Module, Shepard improvised a moment of levity by attaching a 6-iron head to a tool handle and taking two swings at a retrieved , demonstrating the low-gravity environment with the ball traveling several meters. This activity, captured on video, highlighted human adaptability amid the mission's scientific rigor while underscoring the EVA's success in contributing to the total of 42.9 kilograms of samples collected during the mission despite the obstacles.

Lunar Module Ascent

The ascent of the Apollo 14 Antares from the Fra Mauro highlands occurred on February 6, 1971, at 1:48 p.m. EST, corresponding to a ground elapsed time (GET) of 141 hours 45 minutes. The liftoff sequence began with an ullage burn using the ascent stage (RCS) thrusters to settle propellants, followed immediately by ignition of the ascent propulsion system (APS) . The APS, a hypergolic bipropellant with a nominal of 16,000 N, provided a delta-V of approximately 2,200 m/s during a burn duration of 432 seconds, accelerating the ascent stage from the lunar surface to orbital velocity. Performance data from the powered flight processor and guidance systems aligned closely with pre-mission predictions, confirming nominal operation of both the primary and abort RCS systems throughout the burn. The trajectory followed a direct abort profile, inserting Antares into an initial of approximately 15 by 85 km (9.3 by 59 nautical miles) with no major anomalies. This orbit placed the perilune near the planned 15 km altitude, enabling efficient rendezvous while providing an abort capability if needed. The ascent plume, generated by the APS nozzle at the lunar surface, disturbed and displaced fine regolith dust over a wide area, creating a visible radial observable from orbit; however, this effect did not impact mission objectives or equipment left on the surface. Crew reports and post-flight analysis indicated smooth structural loads and attitude control, with the ascent stage achieving the targeted velocity increment without deviations exceeding 0.1 percent. Rendezvous with the Command and Service Module Kitty Hawk employed a direct sequence involving four midcourse burns using the RCS thrusters: two constant differential height (CDH) maneuvers to adjust the and height, followed by terminal phase initiation (TPI) at approximately 2 km separation, and final corrections for station-keeping and approach. The TPI burn delivered a delta-V of about 19 m/s over 3 to 4 seconds, positioning Antares on a collision course for docking. Docking was achieved at GET 143 hours 32 minutes (approximately 1 hour 47 minutes after liftoff), with the probe-and-drogue mechanism engaging nominally after a brief period of station-keeping. After hard dock and tunnel pressurization, Commander and Lunar Module Pilot transferred roughly 43 kg of lunar rock and soil samples, along with exposed film magazines from surface documentation, to Kitty Hawk for return to . The ascent stage was then jettisoned at approximately 145 hours GET, initiating a targeted impact on the to support passive seismic experiments; Command Module Pilot visually confirmed the separation and departing trajectory from Kitty Hawk's window, reporting a clear view of the LM against the lunar horizon.

Command Module Operations

Roosa's Lunar Orbit Activities

During the approximately 33-hour lunar surface stay by astronauts and from February 5 to 6, 1971, Command Module Pilot Stuart A. Roosa operated solo in the Command and Service Module Kitty Hawk, completing a total of 34 orbits over 2 days, 18 hours, and 35 minutes. Roosa's primary responsibilities included maintaining position and preparing for the rendezvous, while managing routine operations in isolation. Roosa executed several key orbit adjustment maneuvers to ensure stable flight parameters. These included a circularization burn of approximately 4 seconds using the Service Propulsion System (SPS) at 105:11:46 mission elapsed time (MET) to maintain a ~60 following Lunar Module separation. Additionally, he conducted an 18.5-second plane change burn using the (RCS) at 117:29:33 MET to adjust the by 1.3 degrees, aligning Kitty Hawk for the efficient rendezvous with the ascending Lunar Module after its surface operations. These maneuvers demanded precise piloting to conserve and position the correctly, drawing on the Command and Service Module's advanced capabilities. For visual observations, Roosa used a handheld 70mm Hasselblad camera to capture high-resolution photographs of approximately 20 candidate landing sites for future Apollo missions, including detailed imaging of the Tycho crater's central peak and blanket for geological analysis, as well as the proposed site in the . These photographs provided critical reconnaissance data, with Roosa noting clear views of lunar features during his passes, such as the bright rays emanating from Tycho. Amid these tasks, Roosa handled essential duties, continuously monitoring vital systems like power, control, and to ensure health. He consumed rehydrated meals, including fruit and cereal packs, and scheduled brief sleep periods, though his packed timeline—often 16 hours of activity per day—limited rest to short naps strapped into the couch. Psychologically, the isolation of solo orbit, with periods of darkness and silence behind the , presented challenges, but Roosa later described it as manageable due to the demanding workload: "Well, actually I was so busy that you really didn't have time to consider the fact that you're by yourself." Roosa remained on alert for potential contingencies, particularly if Antares encountered ascent issues, maintaining readiness to execute an emergency direct rendezvous trajectory using the SPS engine. He conducted regular communications with Mission Control in , relaying status updates during acquisition of signal windows and confirming orbital data to support surface operations, ensuring seamless coordination throughout the isolation period.

Scientific Experiments from Orbit

During the Apollo 14 mission, Command Module Pilot Stuart A. Roosa conducted several lunar orbital experiments designed to investigate the Moon's , surface properties, and , primarily using instruments mounted in the Command and Service Module's Scientific Instrument Module bay. These included the S-band transponder experiment (S-161), which measured Doppler shifts in radio signals to detect mass concentrations (mascons) beneath the lunar surface, confirming their presence in major basins like Imbrium and providing data on gravitational anomalies that influenced orbital trajectories. The downlink experiment (S-160) transmitted signals from the that reflected off the lunar surface and were received back on , yielding insights into , properties, and characteristics, particularly over the Fra Mauro region, where it revealed variations in composition consistent with highland . A laser altimeter (S-164) was also deployed to measure the spacecraft's altitude above the lunar surface with an accuracy of about 10 meters, generating topographic profiles that supported the identification of mascons by correlating elevation changes with and highlighting subtle undulations in the Fra Mauro highlands. These measurements contributed to an improved understanding of the Moon's irregular , with results indicating mascon-induced perturbations on the order of 0.01-0.02 m/s² in certain orbits. Orbital photography formed a core component of the scientific payload, utilizing the Fairchild mapping camera (S-162) to capture high-resolution images of the lunar near side. The camera, operating at a resolution of approximately 20 meters from a 110 km orbit, produced approximately 469 usable frames covering key areas including the Fra Mauro formation and potential future landing sites, enabling detailed mapping of geologic features such as craters, ridges, and blankets, despite a malfunction that caused overexposure. These images documented variations across the highlands, with brighter from Cone Crater contrasting against darker units, providing evidence for the Imbrium impact's role in shaping Fra Mauro's stratified . Overall, these orbital observations, analyzed post-mission, reinforced the ejecta origin of the Fra Mauro formation and provided baseline data for correlating surface samples with regional geology.

Return to Earth

Transearth Injection

The Transearth Injection (TEI) maneuver for Apollo 14 was executed using the Command and Service Module's (CSM) Service Propulsion Subsystem (SPS) engine at a Ground Elapsed Time (GET) of 148:36 on February 7, 1971. The burn imparted a delta-V of 1,055 m/s (3,460 ft/s), raising the perilune altitude to 107 km (66.5 miles) and achieving an outbound velocity of 2.59 km/s (8,505 ft/s) relative to the Moon. Following the TEI burn, the CSM departed lunar orbit on a free-return trajectory toward . Two midcourse corrections were planned during the transearth coast phase, with a total delta-V of 3 m/s, though only one was ultimately required and performed using the approximately 17 hours after TEI to refine the entry corridor. During the approximately three-day coast back to Earth, the crew engaged in detailed debriefings with Mission Control to review mission events, cataloged the lunar samples for scientific processing, and captured television broadcasts of the growing , marred only by a minor failure in the television system that affected signal quality. The spacecraft's relied on crew-conducted sightings for attitude updates and continuous ground tracking from -based stations, resulting in no significant trajectory errors or deviations from the predicted path.

Reentry and Splashdown

The command module Kitty Hawk commenced reentry into Earth's atmosphere on February 9, 1971, at approximately 3:25 p.m. EST, corresponding to a mission elapsed time of 215 hours 27 minutes. The entry interface occurred at an angle of -6.5 degrees, with the spacecraft traveling at a of about 24,500 miles per hour. To maintain aerodynamic stability during the high-speed descent, the crew executed rotation maneuvers to align the command module in the proper lift vector orientation prior to blackout. Peak deceleration reached 6.2 g's, subjecting astronauts , , and to significant but tolerable forces as the ablative dissipated frictional heat. The command module splashed down in the South Pacific Ocean at 4:05 p.m. EST, approximately 765 nautical miles south of and 4 miles from the prime recovery ship USS New Orleans. The impact velocity was approximately 3.6 meters per second under three main parachutes, resulting in a landing offset of about 1.02 nautical miles from the planned target point. Recovery operations began immediately, with a U.S. helicopter from the USS New Orleans hoisting the crew via swimmer-assisted extraction from the stabilization raft. Aboard the ship, the astronauts received thorough medical evaluations, confirming all three were in excellent health with no adverse effects from the mission or reentry. procedures were initiated on the vessel to prevent potential lunar contaminant spread, in line with post-mission protocols. Examination of the command module post-recovery showed minor ablation on the ablative heat shield, as expected from atmospheric friction, with no damage to the structure or systems.

Post-Mission Analysis

Sample Analysis and Scientific Findings

The Apollo 14 mission returned 42.8 kilograms of lunar material to , consisting of 95 rocks and extensive samples collected primarily from the Fra Mauro Formation and the blanket of Cone Crater. Among these, breccias formed the majority, with many sourced from the Cone Crater rim, revealing complex impact histories; high-resolution U-Pb dating of calcium phosphates within these breccias confirmed they represent from the Imbrium basin impact approximately 3.9 billion years ago, providing evidence for the formation of multi-ring basins during the Moon's early period. Surface features on the samples, such as zap pits—small craters (typically 1-100 micrometers in ) caused by impacts—offered insights into the flux and energy of interplanetary dust particles over billions of years, with densities varying from 10 to 100 pits per square centimeter on exposed rock faces. Data from the Apollo Lunar Surface Experiments Package (ALSEP) deployed at the Fra Mauro site yielded significant geophysical and environmental measurements. Active and passive seismic experiments detected waves from both natural moonquakes and controlled thumper detonations, indicating a layer thickness of 8 to 12 meters overlying fractured , with seismic velocities increasing from about 100 m/s in the loose surface material to over 300 m/s at depth. The Suprathermal Ion Detector Experiment (SIDE) within ALSEP measured positive s in the lunar exosphere, revealing enrichment in from implantation, with concentrations up to 10-20 parts per billion in surface soils, reflecting long-term exposure and offering clues to the Sun's isotopic evolution over 4 billion years. Additionally, SIDE observations of ion fluxes, including sporadic bursts of ions (H+), provided the first direct evidence of a tenuous lunar influenced by interactions and plasma processes. Orbital operations by command module pilot supported experiments that complemented surface data. The gamma-ray spectrometer mapped and distributions across the lunar nearside, identifying elevated levels in the highlands consistent with KREEP-rich materials from the Imbrium event, while the spectrometer delineated aluminum-to-silicon ratios for future landing site selection, highlighting Fra Mauro's basaltic underlayer. These datasets, combined with , revealed topographic features tied to ancient basins, aiding in the reconstruction of lunar crustal evolution. More recent analyses, including 2023 geological mapping using (LRO) and Kaguya data, have further refined the stratigraphic context of the Fra Mauro site and its relation to ancient impacts. Post-mission analyses, including reexaminations after 2000 using advanced techniques like secondary ion mass spectrometry, detected trace water (OH and H2O) in Apollo 14 samples, with concentrations ranging from 700 to approximately 2000 ppm in minerals of 14303, suggesting indigenous retained from the Moon's magmatic differentiation rather than solely from cometary delivery. Overall, these findings confirmed the violent impact history shaping the lunar highlands, enriched understanding of implantation processes through isotopic signatures like , and underscored the Moon's dry but not anhydrous primitive state, influencing models of planetary formation.

Mission Outcomes and Lessons Learned

Apollo 14 achieved complete success in meeting all primary and detailed objectives, including selenological inspection, deployment of the Apollo Lunar Surface Experiments Package (ALSEP), and performance of two extravehicular activities (EVAs) in the Fra Mauro highlands. The mission's two EVAs totaled 9 hours and 24 minutes, establishing a new record for cumulative lunar surface time by a landing crew at that point in the program. The Modular Equipment Transporter (MET), a two-wheeled for carrying tools and samples, proved effective in supporting extended traverses of up to 1.4 miles (2.3 km) from the , demonstrating its utility for future mobility enhancements. A critical challenge during the lunar module descent involved intermittent false abort signals triggered by a short circuit in the abort switch circuitry, which threatened to prematurely halt the landing. Mission controllers and the crew implemented an in-flight software workaround by entering a specific sequence into the Apollo Guidance Computer to mask the faulty signal, allowing the landing to proceed safely. This procedure was refined and incorporated into the flight plans for subsequent missions, Apollo 15 through 17, enhancing reliability of the descent phase. Additionally, the mission demonstrated improved landing precision, with the lunar module touching down approximately 27 meters (89 feet) from the targeted site, a significant advancement over prior flights. The mission's accomplishments restored confidence in the Apollo program following the near-disaster of , serving as a pivotal demonstration that complex spaceflight challenges could be overcome through rigorous engineering and operational discipline. By validating extended surface operations and equipment like the MET, Apollo 14 laid essential groundwork for the subsequent J-type missions (–17), which incorporated the for even greater mobility and scientific productivity. Post-mission reviews led to strengthened contingency planning protocols, including more robust simulations and redundant systems checks, directly informed by experiences and applied to ensure safer operations in remaining lunar landings. Lunar dust proved abrasive and pervasive, prompting design improvements in seals, fabrics, and cleaning methods for suits and equipment to mitigate wear and visibility issues in future EVAs. The crew's 21-day upon return yielded no evidence of lunar pathogens, leading to discontinue mandatory post-mission isolation starting with .

Legacy and Artifacts

Mission Insignia and Symbolism

The Apollo 14 mission insignia is an embroidered cloth patch, approximately 3.5 inches in diameter, worn by the astronauts on their spacesuits and flight suits during the mission. It was designed collaboratively by the prime crew—commander Alan B. Shepard Jr., command module pilot Stuart A. Roosa, and lunar module pilot Edgar D. Mitchell—with artistic rendering support from NASA contractors. The circular design features a central gold astronaut pin emblem in stylized flight, arcing upward from a depiction of Earth toward the Moon, set against a black space background to evoke the void of space. Inscribed in white lettering beneath the trajectory is "APOLLO XIV" for the mission designation. The crew's initials—"S," "R," and "M"—appear in white along the lower curve, personalizing the emblem for Shepard, Roosa, and Mitchell. A thin gold border encircles the entire patch, providing a polished, official appearance. Symbolically, the gold pin represents the 's elite status as qualified astronauts, eligible to wear the gold variant of the pin awarded for experience; silver pins were reserved for those yet to fly in space. The upward trajectory from to the Moon illustrates the mission's path and objective to explore the geologically significant Fra Mauro region, chosen for its ancient from the Imbrium impact basin. This design marked the first incorporation of the astronaut pin into an Apollo , a motif that became standard in later emblems to honor qualifications and the exploratory spirit of the program. The simplicity of the elements underscores the mission's focus on reliable execution and scientific return following prior challenges. The underwent a novel approval process, with the crew finalizing and approving the design before submission to for review in late 1970, reversing the typical NASA-led approach for earlier Apollo missions. Patches were sewn onto the astronauts' orange beta suits and white spacesuits, and high-resolution artwork was publicly released in the weeks leading up to the January 31, 1971, launch to build anticipation. As the mission immediately following the aborted Apollo 13 flight, the Apollo 14 insignia embodied themes of resilience and program recovery, resonating with the public and inspiring official NASA merchandise such as medallions, posters, and apparel that celebrated the successful return to the lunar surface.

Spacecraft Locations and Preservation

The Apollo 14 Command Module Kitty Hawk (CSM-110) was recovered from the Pacific Ocean splashdown on February 9, 1971, and has been on public display at the Kennedy Space Center Visitor Complex in Florida since that year. It is housed in the Treasures of NASA Gallery, where it serves as a key artifact illustrating the mission's reentry and recovery operations. The Lunar Module Antares (LM-8) consists of two main components left on the Moon. The descent stage remains at the Fra Mauro landing site, positioned at coordinates 3.64544° S, 17.47139° W, serving as a stable platform that supported the astronauts' surface activities and the deployment of experiments. The ascent stage, after lifting off on February 6, 1971, rendezvoused with the Command Module in before being jettisoned; it impacted the lunar surface on February 7, 1971, at approximately 8° 05' 35" S, 26° 01' 23" W, about 156 miles from the planned target to generate seismic data for the Apollo Passive Seismic Experiment. This impact site has been imaged by the , confirming the crater formation. The launch vehicle (SA-509) for Apollo 14 comprised three stages that were expended during ascent and not recovered for preservation. The first stage (S-IC-9) and second stage (S-II-9) impacted the Atlantic Ocean off the coast of following separation. The third stage (S-IVB-509) performed before being commanded to impact the on February 4, 1971, at coordinates near 8.18° S, 26.03° W in , producing seismic signals detected by the and 14 surface stations; no orbital decay occurred as it was intentionally directed to crash. The impact site has been imaged by the Lunar Reconnaissance Orbiter (LRO), providing high-resolution views as of 2025. Among other mission artifacts, the Apollo Lunar Surface Experiments Package (ALSEP) deployed at Fra Mauro transmitted data until operational anomalies and budget constraints led to its remote shutdown on September 30, 1977, alongside other Apollo ALSEPs. The approximately 43 kilograms of lunar samples returned by Apollo 14 are stored and curated at the Lunar Sample Laboratory Facility at NASA's in , , under controlled nitrogen atmosphere conditions to prevent contamination. A training unit of the Modular Equipment Transporter (MET), a hand-pulled cart used during the extravehicular activities to carry tools and samples, is preserved in the collection of the Smithsonian Institution's , transferred in 1972.

References

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