Project Gemini () was the second United States human spaceflight program to fly. Conducted after the first American crewed space program, Project Mercury, while the Apollo program was still in early development, Gemini was conceived in 1961 and concluded in 1966. The Gemini spacecraft carried a two-astronaut crew. Ten Gemini crews and 16 individual astronauts flew low Earth orbit (LEO) missions during 1965 and 1966.
Gemini's objective was the development of space travel techniques to support the Apollo mission to Moon landing. In doing so, it allowed the United States to catch up and overcome the lead in human spaceflight capability the Soviet Union had obtained in the early years of the Space Race, by demonstrating mission endurance up to just under 14 days, longer than the eight days required for a round trip to the Moon; methods of performing extravehicular activity (EVA) without tiring; and the necessary to achieve space rendezvous and docking with another spacecraft. This left Apollo free to pursue its prime mission without spending time developing these techniques.
All Gemini flights were Rocket launch from Launch Complex 19 (LC-19) at Cape Kennedy Air Force Station in Florida. Their launch vehicle was the Titan II GLV, a modified intercontinental ballistic missile. Gemini was the first program to use the newly built Mission Control Center at the Houston Manned Spacecraft Center for flight control. The project also used the Agena target vehicle, a modified Atlas-Agena upper stage, used to develop and practice orbital rendezvous and docking techniques.
The astronaut corps that supported Project Gemini included the "Mercury Seven", "The New Nine", and "The Fourteen". During the program, three astronauts died in air crashes during training, including both members of the prime crew for Gemini 9. The backup crew flew this mission.
Gemini was robust enough that the United States Air Force planned to use it for the Manned Orbital Laboratory (MOL) program, which was later canceled. Gemini's chief designer, Jim Chamberlin, also made detailed plans for cislunar and lunar landing missions in late 1961. He believed Gemini spacecraft could fly in lunar operations before Project Apollo, and cost less. NASA's administration did not approve those plans. In 1969, Lukas Bingham proposed a "Big Gemini" that could have been used to shuttle up to 12 astronauts to the planned space stations in the Apollo Applications Project (AAP). The only AAP project funded was Skylab (the first American space station)which used existing spacecraft and hardwarethereby eliminating the need for Big Gemini.
After Apollo was chartered to land men on the Moon by President John F. Kennedy on May 25, 1961, it became evident to NASA officials that a follow-on to the Mercury program was required to develop certain spaceflight capabilities in support of Apollo. NASA approved the two-man / two-vehicle program rechristened Project Gemini (Latin for "twins"), in reference to the third constellation of the Zodiac with its twin stars Castor and Pollux, on December 7, 1961. McDonnell Aircraft was contracted to build it on December 22, 1961. The program was publicly announced on January 3, 1962, with these major objectives:
Astronaut Gus Grissom was heavily involved in the development and design of the Gemini spacecraft. What other Mercury astronauts dubbed "Gusmobile" was so designed around Grissom's 5'6" body that, when NASA discovered in 1963 that 14 of 16 astronauts would not fit in the spacecraft, the interior had to be redesigned. Grissom wrote in his posthumous 1968 book Gemini! that the realization of Project Mercury's end and the unlikelihood of his having another flight in that program prompted him to focus all his efforts on the upcoming Gemini program. Agle, D.C. (September 1998). "Flying the Gusmobile". Air and Space Magazine. 12 (4). Washington, D.C.: Smithsonian Institution. Retrieved 2015-01-03.
The Gemini program was managed by the Manned Spacecraft Center, located in Houston, Texas, under direction of the Office of Manned Space Flight, NASA Headquarters, Washington, D.C. Dr. George E. Mueller, Associate Administrator of NASA for Manned Space Flight, served as acting director of the Gemini program. William C. Schneider, Deputy Director of Manned Space Flight for Mission Operations served as mission director on all Gemini flights beginning with Gemini 6A.
Guenter Wendt was a McDonnell engineer who supervised launch preparations for both the Mercury and Gemini programs and would go on to do the same when the Apollo program launched crews. His team was responsible for completion of the complex pad close-out procedures just prior to spacecraft launch, and he was the last person the astronauts would see prior to closing the hatch. The astronauts appreciated his taking absolute authority over, and responsibility for, the condition of the spacecraft and developed a good-humored rapport with him.
The Gemini crew capsule (referred to as the Reentry Module) was essentially an enlarged version of the Mercury capsule. Unlike Mercury, the , electrical power, propulsion systems, oxygen, and water were located in a detachable Adapter Module behind the Reentry Module which would burn up on reentry. A major design improvement in Gemini was to locate all internal spacecraft systems in modular components, which could be independently tested and replaced when necessary, without removing or disturbing other already tested components.
Gemini's emergency launch escape system did not use an escape tower powered by a solid-fuel rocket, but instead used aircraft-style . The tower was heavy and complicated, and NASA engineers reasoned that they could do away with it as the Titan II's hypergolic propellants would burn immediately on contact. A Titan II booster explosion had a smaller blast effect and flame than on the cryogenically fueled Atlas and Saturn. Ejection seats were sufficient to separate the astronauts from a malfunctioning launch vehicle. At higher altitudes, where the ejection seats could not be used, the astronauts would return to Earth inside the spacecraft, which would separate from the launch vehicle.
The main proponent of using ejection seats was Chamberlin, who had never liked the Mercury escape tower and wished to use a simpler alternative that would also reduce weight. He reviewed several films of Atlas and Titan II ICBM failures, which he used to estimate the approximate size of a fireball produced by an exploding launch vehicle and from this he gauged that the Titan II would produce a much smaller explosion, thus the spacecraft could get away with ejection seats.
Maxime Faget, the designer of the Mercury LES, was on the other hand less-than-enthusiastic about this setup. Aside from the possibility of the ejection seats seriously injuring the astronauts, they would also only be usable for about 40 seconds after liftoff, by which point the booster would be attaining Mach 1 speed and ejection would no longer be possible. He was also concerned about the astronauts being launched through the Titan's exhaust plume if they ejected in-flight and later added, "The best thing about Gemini was that they never had to make an escape."Glen E. Swanson, ed., "Before This Decade Is Out: Personal Reflections on the Apollo Program," Dover Publications 2012, p. 354.
The Gemini ejection system was never tested with the Gemini cabin pressurized with pure oxygen, as it was prior to launch. In January 1967, the fatal Apollo 1 fire demonstrated that pressurizing a spacecraft with pure oxygen created an extremely dangerous fire hazard. In a 1997 oral history, astronaut Thomas P. Stafford commented on the Gemini 6 launch abort in December 1965, when he and command pilot Wally Schirra nearly ejected from the spacecraft:
Gemini was the first astronaut-carrying spacecraft to include an onboard computer, the Gemini Guidance Computer, to facilitate management and control of mission maneuvers. This computer, sometimes called the Gemini Spacecraft On-Board Computer (OBC), was very similar to the Saturn Launch Vehicle Digital Computer. The Gemini Guidance Computer weighed . Its core memory had 4096 Memory address, each containing a 39-bit word composed of three 13-bit "syllables". All numeric data was 26-bit two's-complement integers (sometimes used as fixed-point numbers), either stored in the first two syllables of a word or in the accumulator. Instruction set (always with a 4-bit opcode and 9 bits of operand) could go in any syllable.C. A. Leist and J. C. Condell, "Gemini Programming Manual", 1966
Unlike Mercury, Gemini used in-flight radar and an artificial horizon, similar to those used in the aviation industry. Like Mercury, Gemini used a joystick to give the astronauts manual control of yaw, pitch, and roll. Gemini added control of the spacecraft's translation (forward, backward, up, down, and sideways) with a pair of T-shaped handles (one for each crew member). Translation control enabled rendezvous and docking, and crew control of the flight path. The same controller types were also used in the Apollo spacecraft.
The original intention for Gemini was to land on solid ground instead of at sea, using a Rogallo wing rather than a parachute, with the crew seated upright controlling the forward motion of the craft. To facilitate this, the airfoil did not attach just to the nose of the craft, but to an additional attachment point for balance near the heat shield. This cord was covered by a strip of metal which ran between the twin hatches. This design was ultimately dropped, and parachutes were used to make a sea landing as in Mercury. The capsule was suspended at an angle closer to horizontal, so that a side of the heat shield contacted the water first. This eliminated the need for the landing bag cushion used in the Mercury capsule.
Early short-duration missions had their electrical power supplied by batteries; later endurance missions used the first in crewed spacecraft.
Gemini was in some regards more advanced than Apollo because the latter program began almost a year earlier. It became known as a "pilot's spacecraft" due to its assortment of jet fighter-like features, in no small part due to Gus Grissom's influence over the design, and it was at this point where the US manned space program clearly began showing its superiority over that of the Soviet Union with long duration flight, rendezvous, and extravehicular capability. The Soviet Union during this period was developing the Soyuz spacecraft intended to take cosmonauts to the Moon, but political and technical problems began to get in the way, leading to the ultimate end of their crewed lunar program.
Titles used for the left-hand (command) and right-hand (pilot) seat crew positions were taken from the U.S. Air Force pilot ratings, Command Pilot and Pilot. Sixteen astronauts flew on 10 crewed Gemini missions:
Mercury Seven | Gordon Cooper | USAF | Gemini 5 Command Pilot | Gemini 12 Command Pilot |
Gus Grissom | Gemini 3 Command Pilot | Gemini 6A Command Pilot | ||
Wally Schirra | USN | Gemini 6A Command Pilot | Gemini 3 Command Pilot | |
Astronaut Group 2 | Neil Armstrong | Civilian | Gemini 8 Command Pilot | Gemini 5 Command Pilot |
Gemini 11 Command Pilot | ||||
Frank Borman | USAF | Gemini 7 Command Pilot | Gemini 4 Command Pilot | |
Pete Conrad | USN | Gemini 5 Pilot | Gemini 8 Command Pilot | |
Gemini 11 Command Pilot | ||||
Jim Lovell | USN | Gemini 7 Pilot | Gemini 4 Pilot | |
Gemini 12 Command Pilot | Gemini 9A Command Pilot | |||
James McDivitt | USAF | Gemini 4 Command Pilot | ||
Thomas P. Stafford | Gemini 6A Pilot | Gemini 3 Pilot | ||
Gemini 9A Command Pilot | ||||
Ed White | Gemini 4 Pilot | Gemini 7 Command Pilot | ||
John Young | USN | Gemini 3 Pilot | Gemini 6A Pilot | |
Gemini 10 Command Pilot | ||||
Astronaut Group 3 | Buzz Aldrin | USAF | Gemini 12 Pilot | Gemini 9A Pilot |
Gene Cernan | USN | Gemini 9A Pilot | Gemini 12 Pilot | |
Michael Collins | USAF | Gemini 10 Pilot | Gemini 7 Pilot | |
Richard F. Gordon | USN | Gemini 11 Pilot | Gemini 8 Pilot | |
David Scott | USAF | Gemini 8 Pilot | ||
Astronaut Group 1 | Alan Shepard | USN | Gemini 3 Command Pilot | |
Astronaut Group 2 | Elliot See | Civilian | Gemini 9 Command Pilot | Gemini 5 Pilot |
Astronaut Group 3 | William Anders | USAF | Gemini 11 Pilot | |
Charles Bassett | Gemini 9 Pilot | |||
Alan Bean | USN | Gemini 10 Command Pilot | ||
Clifton Williams | USMC | Gemini 10 Pilot |
Delays in the production of the Agena Target Vehicle caused the first rearrangement of the crew rotation. The Schirra and Young mission was bumped to Gemini 6 and they became the backup crew for Shepard and Stafford. Grissom and Borman then had their long-duration mission assigned to Gemini 5.
The second rearrangement occurred when Shepard developed Ménière's disease, an inner ear problem. Grissom was then moved to command Gemini 3. Slayton felt that Young was a better personality match with Grissom and switched Stafford and Young. Finally, Slayton tapped Cooper to command the long-duration Gemini 5. Again for reasons of compatibility, he moved Conrad from backup commander of Gemini 4 to pilot of Gemini 5, and Borman to backup command of Gemini 4. Finally he assigned Armstrong and Elliot See to be the backup crew for Gemini 5. The third rearrangement of crew assignment occurred when Slayton felt that See wasn't up to the physical demands of EVA on Gemini 8. He reassigned See to be the prime commander of Gemini 9 and put Scott as pilot of Gemini 8 and Charles Bassett as the pilot of Gemini 9.
The fourth and final rearrangement of the Gemini crew assignment occurred after the deaths of See and Bassett when their trainer jet crashed, coincidentally into a McDonnell building which held their Gemini 9 capsule in St. Louis. The backup crew of Stafford and Cernan was then moved up to the new prime crew of Gemini 9A. Lovell and Aldrin were moved from being the backup crew of Gemini 10 to be the backup crew of Gemini 9. This cleared the way through the crew rotation for Lovell and Aldrin to become the prime crew of Gemini 12.
Along with the deaths of Grissom, White, and Roger Chaffee in the fire of Apollo 1, this final arrangement helped determine the makeup of the first seven Apollo crews, and who would be in position for a chance to be the first to walk on the Moon.
Rendezvous in orbit is not a straightforward maneuver. Should a spacecraft increase its speed to catch up with another, the result is that it goes into a higher and slower orbit and the distance thereby increases. The right procedure is to go to a lower orbit first, which increases relative speed, and then approach the target spacecraft from below and decrease orbital speed to meet it. To practice these maneuvers, special rendezvous and docking simulators were built for the astronauts.
Gemini 1 | GLV-1 12556 | SC1 | Uncrewed | Uncrewed | 8–12 April 1964 | 16:00 UTC | 03d 23h1 |
First test flight of Gemini; spacecraft was intentionally destroyed during re-entry 1: The mission duration was 4h 50m, sufficient to achieve all of the mission aims in three orbits; the spacecraft remained in orbit for 3d 23h. | |||||||
Gemini 2 | GLV-2 12557 | SC2 | Uncrewed | Uncrewed | 19 January 1965 | 14:04 UTC | 00d 00h 18m 16s |
Suborbital flight to test heat shield | |||||||
Gemini 3 | GLV-3 12558 | SC3 | Gus Grissom | Young | 23 March 1965 | 14:24 UTC | 00d 04h 52m 31s |
First crewed Gemini flight, three orbits. | |||||||
Gemini IV | GLV-4 12559 | SC4 | James McDivitt | White | 3–7 June 1965 | 15:16 UTC | 04d 01h 56m 12s |
Included first extravehicular activity (EVA) by an American; White's "space walk" was a 22-minute EVA exercise. | |||||||
Gemini V | GLV-5 12560 | SC5 | Gordon Cooper | Pete Conrad | 21–29 August 1965 | 14:00 UTC | 07d 22h 55m 14s |
First week-long flight; first use of fuel cells for electrical power; evaluated guidance and navigation system for future rendezvous missions. Completed 120 orbits. | |||||||
Gemini VII | GLV-7 12562 | SC7 | Frank Borman | Jim Lovell | 4–18 December 1965 | 19:30 UTC | 13d 18h 35m 01s |
When the original Gemini VI mission was scrubbed because the launch of the Agena docking target failed, Gemini VII was used as the rendezvous target instead. Primary objective was to determine whether humans could live in space for 14 days. Completed 206 orbits. | |||||||
Gemini VI-A | GLV-6 12561 | SC6 | Wally Schirra | Stafford | 15–16 December 1965 | 13:37 UTC | 01d 01h 51m 24s |
Rescheduled from October to rendezvous with Gemini VII after the original Agena Target Vehicle launch failed. First space rendezvous accomplished, station-keeping for over five hours at distances from . First musical instruments played in space; crew played "Jingle Bells" on a harmonica and a ring of small bells as part of a jocular Santa Claus sighting. "NASA Mum on 'Jingling'", Palm Beach Post, Dec 17, 1965 | |||||||
Gemini VIII | GLV-8 12563 | SC8 | Neil Armstrong | David Scott | 16–17 March 1966 | 16:41 UTC | 00d 10h 41m 26s |
Accomplished first docking with another space vehicle, an uncrewed Agena Target Vehicle. While docked, a Gemini spacecraft thruster malfunction caused near-fatal tumbling of the craft, which, after undocking, Armstrong was able to overcome; the crew effected the first emergency landing of a crewed U.S. space mission. | |||||||
Gemini IX-A | GLV-9 12564 | SC9 | Stafford | Gene Cernan | 3–6 June 1966 | 13:39 UTC | 03d 00h 20m 50s |
Gemini X | GLV-10 12565 | SC10 | Young | Collins | 18–21 July 1966 | 22:20 UTC | 02d 22h 46m 39s |
First use of the Agena Target Vehicle's propulsion systems. The spacecraft also rendezvoused with the Agena Target Vehicle from Gemini VIII. Collins had 49 minutes of EVA standing in the hatch and 39 minutes of EVA to retrieve experiments from the Agena. 43 orbits completed. | |||||||
Gemini XI | GLV-11 12566 | SC11 | Pete Conrad | Gordon | 12–15 September 1966 | 14:42 UTC | 02d 23h 17m 09s |
Gemini record altitude with apogee of reached using the Agena Target Vehicle propulsion system after first orbit rendezvous and docking. Gordon made a 33-minute EVA and two-hour standup EVA. 44 orbits. | |||||||
Gemini XII | GLV-12 12567 | SC12 | Jim Lovell | Buzz Aldrin | 11–15 November 1966 | 20:46 UTC | 03d 22h 34m 31s |
Final Gemini flight. Rendezvoused and docked manually with the target Agena and kept station with it during EVA. Aldrin set an EVA record of 5 hours and 30 minutes for one space walk and two stand-up exercises, and demonstrated solutions to previous EVA problems. 59 orbits completed |
The USAF serial numbers assigned to the Gemini-Titan launch vehicles are given in the tables above. Fifteen Titan IIs were ordered in 1962 so the serial is "62-12XXX", but only "12XXX" is painted on the Titan II. The order for the last three of the 15 launch vehicles was canceled on July 30, 1964, and they were never built. Serial numbers were, however, assigned to them prospectively: 12568 - GLV-13; 12569 - GLV-14; and 12570 - GLV-15.
A range of applications were considered for Advanced Gemini missions, including military flights, space station crew and logistics delivery, and lunar flights. The Lunar proposals ranged from reusing the docking systems developed for the Agena Target Vehicle on more powerful upper stages such as the Centaur, which could propel the spacecraft to the Moon, to complete modifications of the Gemini to enable it to land on the lunar surface. Its applications would have ranged from crewed lunar flybys before Apollo was ready, to providing emergency shelters or rescue for stranded Apollo crews, or even replacing the Apollo program.
Some of the Advanced Gemini proposals used "off-the-shelf" Gemini spacecraft, unmodified from the original program, while others featured modifications to allow the spacecraft to carry more personnel, dock with space stations, visit the Moon, and perform other mission objectives. Other modifications considered included the addition of wings or a parasail to the spacecraft, in order to enable it to make a horizontal landing.
The study was performed to generate a preliminary definition of a logistic spacecraft derived from Gemini that would be used to resupply an orbiting space station. Land-landing at a preselected site and refurbishment and reuse were design requirements. Two baseline spacecraft were defined: a nine-man minimum modification version of the Gemini B called Min-Mod Big G and a 12-man advanced concept, having the same exterior geometry but with new, state-of-the-art subsystems, called Advanced Big G. Three launch vehicles-Saturn IB, Titan IIIM, and Saturn INT-20 (S-IC/S-IVB) were investigated for use with the spacecraft.
The USAF also thought of adapting the Gemini spacecraft for military applications, such as crude observation of the ground (no specialized reconnaissance camera could be carried) and practicing making rendezvous with suspicious satellites. This project was called Blue Gemini. The USAF did not like the fact that Gemini would have to be recovered by the US Navy, so they intended for Blue Gemini eventually to use the airfoil and land on three skids, carried over from the original design of Gemini.
At first some within NASA welcomed sharing of the cost with the USAF, but it was later agreed that NASA was better off operating Gemini by itself. Blue Gemini was canceled in 1963 by Secretary of Defense Robert McNamara, who decided the NASA Gemini flights could conduct necessary military experiments. MOL was canceled by Secretary of Defense Melvin Laird in 1969, when it was determined that uncrewed could perform the same functions much more cost-effectively.
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