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Apollo 5
Apollo 5 (launched January 22, 1968), also known as AS-204, was the uncrewed first flight of the Apollo Lunar Module (LM) that would later carry astronauts to the surface of the Moon. The Saturn IB rocket bearing the LM lifted off from Cape Kennedy on January 22, 1968. The mission was successful, though due to programming problems an alternate mission to that originally planned was executed.
Like Apollo 4, this flight was long delayed, due in part to setbacks in development of the LM, manufactured by Grumman Aircraft. The original Saturn IB rocket that was to take the first LM (LM-1) to space was taken down during the delays and replaced with the one that would have launched Apollo 1 if the spacecraft fire that killed three astronauts had not occurred. LM-1 arrived at the Kennedy Space Center in June 1967; the following months were occupied in testing and placing the LM atop the Saturn IB. After final delays due to equipment trouble, the countdown began on January 21, 1968, and the space vehicle was launched the following day.
Once the craft reached orbit and the LM separated from the S-IVB booster, the program of orbital testing began, but a planned burn was aborted automatically when the Apollo Guidance Computer detected the craft was not going as fast as planned. Flight Director Gene Kranz and his team at Mission Control in Houston quickly decided on an alternate mission, during which the mission's goals of testing LM-1 were accomplished. The mission was successful enough that a contemplated second uncrewed mission to test the LM was cancelled, advancing NASA's plans to land an astronaut on the Moon by the end of the 1960s.
In 1961, United States President John F. Kennedy challenged the United States to land an astronaut on the Moon by the end of the decade, with a safe return to Earth. After considerable debate, NASA (the US government's spaceflight agency) decided in late 1962 that lunar missions would use a lunar orbit rendezvous in which the complete Apollo spacecraft would be propelled towards lunar orbit by the Saturn V launch vehicle's third stage (called the S-IVB). Once in lunar orbit, those astronauts who would land on the Moon would enter what was then called the lunar excursion module (LEM) (later called the lunar module (LM)). This craft would separate from the Apollo's command and service module (CSM) and land on the Moon. When the astronauts were ready to return, they would enter the LM, take off, and re-dock with the CSM. Once the crew reentered the CSM, they would discard the lunar module and return to Earth in the CSM. In 1962, NASA invited eleven companies to bid for the contract to construct the LM. On November 7, 1962, NASA announced that it had awarded the contract to Grumman in Bethpage, New York.
As with Apollo 4, there were significant delays for Apollo 5. The primary cause of the Apollo 5 delays was the LM, which was behind schedule. Apollo Program Manager Major General Samuel C. Phillips had originally hoped that the uncrewed test flight of LM-1, the first lunar module, would launch in April 1967. Anticipating six months for checkout and testing of the vehicle, NASA asked Grumman to have LM-1 delivered to Kennedy Space Center in Florida by September 1966, but due to difficulties in manufacturing LM-1, delivery was repeatedly delayed. The delivery date was still uncertain when AS-206, the Saturn IB launch vehicle planned to boost LM-1 to orbit, was erected at Launch Complex 37 in January 1967. After the fire that month that killed the Apollo 1 crew, the launch vehicle planned for Apollo 1, AS-204, was moved from Launch Complex 34 to Launch Complex 37 and replaced AS-206. This was done because AS-204 was the last Saturn IB with full research and development instrumentation, and, with crewed flight on hold, NASA wanted to use that booster for the first flight of the LM.
With no LM yet available, Grumman built a plywood mockup of one at Launch Complex 37 to aid in facilities verification. On May 12, 1967, Apollo Program Spacecraft Manager George M. Low informed NASA headquarters that Grumman was committed to a June 28 delivery of LM-1, though Low noted that the goal would be hard to meet. On June 23, LM-1 arrived at Cape Kennedy on board Aero Spacelines' Super Guppy; the stages were mated to each other four days later. A 400-person team under John J. Williams, a veteran of launch operations for both Mercury and Gemini, checked to see that LM-1 met specifications, after which they supervised Grumman technicians, who tested and modified the vehicle. Due to leaks in the LM's ascent stage, the two stages were demated in August, and after these were fixed and the stages remated, another leak developed and the stages were demated again in September. During this time, several pieces of equipment were removed for repair by Grumman; the stages were remated again in October.
As of September 6, 1967, Apollo 5 was running about 39 days behind the plan established on July 18, but all known issues were being dealt with, with the exception of some leaks from the propulsion system. Most mission documents were ready by late 1967; Mission Director William C. Schneider issued mission rules on November 18, 1967. The following day, LM-1 was mated to its launch vehicle, and the space vehicle readiness test was completed in December. In early January 1968, the office of NASA Administrator James E. Webb announced that Apollo 5 would be launched no earlier than January 18, 1968. Minor faults such as clogged filters led to some additional delays. The countdown demonstration test concluded on January 19 and an abbreviated 22-hour countdown began on January 21.
Apollo 5 was intended to verify the operation of the subsystems of the LM. During the flight, the ascent and descent engines would be fired. A "fire in the hole" test would be conducted to verify that the ascent stage could still fire while attached to the descent stage, a procedure that would be used on the lunar surface and in the event of an aborted lunar landing. It involved shutting down the descent stage, switching control and power to the ascent stage, and starting the ascent engine while the two stages were still mated. The term "fire in the hole" derived from a term used in mining when explosives are about to be used. Additional testing was to check that the LM engines could be restarted after initial use. In addition to testing LM systems, Apollo 5 was to test the Instrument Unit in its Saturn V configuration.
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Apollo 5
Apollo 5 (launched January 22, 1968), also known as AS-204, was the uncrewed first flight of the Apollo Lunar Module (LM) that would later carry astronauts to the surface of the Moon. The Saturn IB rocket bearing the LM lifted off from Cape Kennedy on January 22, 1968. The mission was successful, though due to programming problems an alternate mission to that originally planned was executed.
Like Apollo 4, this flight was long delayed, due in part to setbacks in development of the LM, manufactured by Grumman Aircraft. The original Saturn IB rocket that was to take the first LM (LM-1) to space was taken down during the delays and replaced with the one that would have launched Apollo 1 if the spacecraft fire that killed three astronauts had not occurred. LM-1 arrived at the Kennedy Space Center in June 1967; the following months were occupied in testing and placing the LM atop the Saturn IB. After final delays due to equipment trouble, the countdown began on January 21, 1968, and the space vehicle was launched the following day.
Once the craft reached orbit and the LM separated from the S-IVB booster, the program of orbital testing began, but a planned burn was aborted automatically when the Apollo Guidance Computer detected the craft was not going as fast as planned. Flight Director Gene Kranz and his team at Mission Control in Houston quickly decided on an alternate mission, during which the mission's goals of testing LM-1 were accomplished. The mission was successful enough that a contemplated second uncrewed mission to test the LM was cancelled, advancing NASA's plans to land an astronaut on the Moon by the end of the 1960s.
In 1961, United States President John F. Kennedy challenged the United States to land an astronaut on the Moon by the end of the decade, with a safe return to Earth. After considerable debate, NASA (the US government's spaceflight agency) decided in late 1962 that lunar missions would use a lunar orbit rendezvous in which the complete Apollo spacecraft would be propelled towards lunar orbit by the Saturn V launch vehicle's third stage (called the S-IVB). Once in lunar orbit, those astronauts who would land on the Moon would enter what was then called the lunar excursion module (LEM) (later called the lunar module (LM)). This craft would separate from the Apollo's command and service module (CSM) and land on the Moon. When the astronauts were ready to return, they would enter the LM, take off, and re-dock with the CSM. Once the crew reentered the CSM, they would discard the lunar module and return to Earth in the CSM. In 1962, NASA invited eleven companies to bid for the contract to construct the LM. On November 7, 1962, NASA announced that it had awarded the contract to Grumman in Bethpage, New York.
As with Apollo 4, there were significant delays for Apollo 5. The primary cause of the Apollo 5 delays was the LM, which was behind schedule. Apollo Program Manager Major General Samuel C. Phillips had originally hoped that the uncrewed test flight of LM-1, the first lunar module, would launch in April 1967. Anticipating six months for checkout and testing of the vehicle, NASA asked Grumman to have LM-1 delivered to Kennedy Space Center in Florida by September 1966, but due to difficulties in manufacturing LM-1, delivery was repeatedly delayed. The delivery date was still uncertain when AS-206, the Saturn IB launch vehicle planned to boost LM-1 to orbit, was erected at Launch Complex 37 in January 1967. After the fire that month that killed the Apollo 1 crew, the launch vehicle planned for Apollo 1, AS-204, was moved from Launch Complex 34 to Launch Complex 37 and replaced AS-206. This was done because AS-204 was the last Saturn IB with full research and development instrumentation, and, with crewed flight on hold, NASA wanted to use that booster for the first flight of the LM.
With no LM yet available, Grumman built a plywood mockup of one at Launch Complex 37 to aid in facilities verification. On May 12, 1967, Apollo Program Spacecraft Manager George M. Low informed NASA headquarters that Grumman was committed to a June 28 delivery of LM-1, though Low noted that the goal would be hard to meet. On June 23, LM-1 arrived at Cape Kennedy on board Aero Spacelines' Super Guppy; the stages were mated to each other four days later. A 400-person team under John J. Williams, a veteran of launch operations for both Mercury and Gemini, checked to see that LM-1 met specifications, after which they supervised Grumman technicians, who tested and modified the vehicle. Due to leaks in the LM's ascent stage, the two stages were demated in August, and after these were fixed and the stages remated, another leak developed and the stages were demated again in September. During this time, several pieces of equipment were removed for repair by Grumman; the stages were remated again in October.
As of September 6, 1967, Apollo 5 was running about 39 days behind the plan established on July 18, but all known issues were being dealt with, with the exception of some leaks from the propulsion system. Most mission documents were ready by late 1967; Mission Director William C. Schneider issued mission rules on November 18, 1967. The following day, LM-1 was mated to its launch vehicle, and the space vehicle readiness test was completed in December. In early January 1968, the office of NASA Administrator James E. Webb announced that Apollo 5 would be launched no earlier than January 18, 1968. Minor faults such as clogged filters led to some additional delays. The countdown demonstration test concluded on January 19 and an abbreviated 22-hour countdown began on January 21.
Apollo 5 was intended to verify the operation of the subsystems of the LM. During the flight, the ascent and descent engines would be fired. A "fire in the hole" test would be conducted to verify that the ascent stage could still fire while attached to the descent stage, a procedure that would be used on the lunar surface and in the event of an aborted lunar landing. It involved shutting down the descent stage, switching control and power to the ascent stage, and starting the ascent engine while the two stages were still mated. The term "fire in the hole" derived from a term used in mining when explosives are about to be used. Additional testing was to check that the LM engines could be restarted after initial use. In addition to testing LM systems, Apollo 5 was to test the Instrument Unit in its Saturn V configuration.
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