Gemini 11

Gemini XI
	Gemini XI conducting a tether experiment using the Agena Target Vehicle
Mission type	Space rendezvous; Spacecraft docking; Extravehicular activity;
Operator	NASA
COSPAR ID	1966-081A
SATCAT no.	2415
Mission duration	2 days 23 hours 17 minutes 9 seconds
Orbits completed	44
Spacecraft properties
Spacecraft	Gemini SC11
Manufacturer	McDonnell
Launch mass	3,798 kilograms (8,374 lb)
Landing mass	1,920 kilograms (4,230 lb)
Crew
Crew size	2
Members	Charles "Pete" Conrad Jr.; Richard F. Gordon Jr.;
EVAs	2
EVA duration	2 hours 41 minutes
Start of mission
Launch date	September 12, 1966, 14:42:26 UTC
Rocket	Titan II GLV
Launch site	Cape Kennedy LC-19
End of mission
Recovered by	USS Guam
Landing date	September 15, 1966, 13:59:35 UTC
Landing site	24°15′N 70°0′W / 24.250°N 70.000°W
Orbital parameters
Reference system	Geocentric
Regime	Low Earth orbit
Perigee altitude	298 kilometers (161 nmi)
Apogee altitude	1,368 kilometers (739 nmi)
Inclination	28.8 degrees
Period	101.57 minutes
Epoch	September 14, 1966
Docking with GATV-5006
Docking date	September 12, 1966, 16:16:00 UTC
Undocking date	September 14, 1966, 16:55:00 UTC
Time docked	2 days 39 minutes
	; Gordon (left) and Conrad Project Gemini ← Gemini 10 Gemini 12 →

Gemini 11 (officially Gemini XI)^[2] was the ninth crewed spaceflight mission of NASA's Project Gemini, which flew from September 12 to 15, 1966. It was the 17th crewed American flight and the 25th spaceflight to that time (includes X-15 flights over 100 kilometers (54 nmi)). Astronauts Charles "Pete" Conrad Jr. and Richard F. Gordon Jr. performed the first direct-ascent (first orbit) rendezvous with an Agena Target Vehicle, docking with it 1 hour 34 minutes after launch; used the Agena rocket engine to achieve a record high-apogee Earth orbit; and created a small amount of artificial gravity by spinning the two spacecraft connected by a tether. Gordon also performed two extra-vehicular activities for a total of 2 hours 41 minutes.

Crew[edit]


Position	Astronaut
Command Pilot	Charles "Pete" Conrad Jr. Second spaceflight
Pilot	Richard F. Gordon Jr. First spaceflight

Backup crew[edit]


Position	Astronaut
Command Pilot	Neil A. Armstrong
Pilot	William A. Anders

Support crew[edit]

Clifton C. Williams Jr. (Cape CAPCOM)
John W. Young (Houston CAPCOM)
Alan L. Bean (Houston CAPCOM)

Mission parameters[edit]

Mass: 8,374 pounds (3,798 kg)

Highest orbit (followed twice):

Perigee: 156.4 nautical miles (289.7 km)
Apogee: 739.2 nautical miles (1,369.0 km)^[3]
Inclination: 28.85°
Period: 101.52 min

Docking[edit]

Docked: September 12, 1966, 16:16:00 UTC
Undocked: September 14, 1966, 16:55:00 UTC

Space walk[edit]

Gordon – EVA 1
- Start: September 13, 1966, 14:44:00 UTC
- End: September 13, 1966, 15:17:00 UTC
- Duration: 0 hours 33 minutes
Gordon – EVA 2 (stand up)
- Start: September 14, 1966, 12:49:00 UTC
- End: September 14, 1966, 14:57:00 UTC
- Duration: 2 hours 08 minutes

Objectives[edit]

Perform a direct-ascent rendezvous with the Agena Target Vehicle on the first orbit in support of Project Apollo. This would simulate a Lunar Module rendezvous with the Command/Service Module after a lunar landing.
Use the Agena rocket engine to put the combined craft in a high-apogee elliptical orbit.
Perform two extra-vehicular activities.
Demonstrate passive attitude stabilization of the two spacecraft connected by a tether and create artificial gravity by spinning the combined craft.^[4]
Perform miscellaneous scientific experiments.
Perform a computer-controlled atmospheric reentry to a precision splashdown point.

Gemini 11	Agena info
Agena	GATV-5006
NSSDC ID:	1966-080A
Mass	7,000 pounds (3,200 kg)
Launch site	LC-14
Launch date	September 12, 1966
Launch time	13:05:01 UTC
1st perigee	156.4 nautical miles (289.7 km)
1st apogee	165.8 nautical miles (307.1 km)
Period	90.56 min
Inclination	28.84 deg
Reentered	December 30, 1966

Flight[edit]

Arabian Peninsula (top left) and northeast Africa (bottom) as seen from the orbiting Gemini-11 spacecraft at an altitude of 340 nautical miles during its 27th revolution around Earth. (Taken with a modified 70 mm Hasselblad camera.)

The direct-ascent rendezvous and docking with the Agena vehicle was achieved approximately 94 minutes after lift-off, depending on the on-board computer and radar equipment with only minimal assistance from ground support.^[4]

Gemini 11 used the rocket on its Agena target vehicle to raise its apogee to 853 miles (1,373 km), the highest Earth orbit ever reached by a crewed spacecraft.^[5] The perigee was 179 miles (288 km), and maximum velocity (at perigee) was 17,967 miles per hour (28,915 km/h).^[4] The apogee record stands as of October 2022, even though men have achieved greater distances from Earth by flying to the Moon in the Apollo program.^[6] The maximum operational altitude of the Space Shuttle was much lower, at 386 miles (621 km) for the STS-31 flight in 1990. The September 2021 SpaceX flight of Inspiration4, while having an apogee higher than most Space Shuttle flights, only reached 585 kilometres (364 mi).^[7]

The crew docked and undocked four times and still had sufficient Gemini maneuvering fuel for an unplanned fifth rendezvous. They did not remain in the high orbit, but changed it back to a near-circular one at 184 miles (296 km).^[4]

Gordon's first EVA, planned to last for two hours, involved fastening a 100-foot (30 m) tether, stored in the Agena's docking collar, to the Gemini's docking bar for the passive stabilization experiment. Gordon achieved this, but as with previous Gemini EVAs, trying to do work for an extended period proved more fatiguing than in ground simulation, and the EVA had to be terminated after only half an hour.

The passive stabilization experiment proved to be a bit troublesome. Conrad and Gordon separated the craft in a nose-down (i.e., Agena-down) position, but found that the tether would not be kept taut simply by the Earth's gravity gradient, as expected. However, they were able to generate a small amount of artificial gravity, about 0.00015 g, by firing their side thrusters to slowly rotate the combined craft like a slow-motion pair of bolas.^[4]

Gordon successfully performed a second EVA standing up with his head and shoulders out of the hatch to photograph the Earth, clouds, and stars. This was not tiring and lasted more than two hours.^[4]

Scientific experiments[edit]

The 12 scientific experiments were:^[8]

Mass Determination: To test a technique and accuracy of a direct-contact method of determining the mass of an orbiting object, in this case the Agena Target Vehicle.
Night Image Intensification: To test the usefulness and performance of a low-light-level television system as a supplement to unaided vision in observing surface features primarily when such features are in darkness and spacecraft pilots are not dark-adapted.
Power Tool Evaluation: To evaluate man's capability to perform work tasks in space, including the comparison of ability to work tethered and untethered, and to evaluate the performance of the minimum-reaction power tool.
Radiation and Zero G Effects on Blood and Neurospora: To determine whether weightlessness enhances the effects of radiation on human white blood cells and Neurospora crassa fungi.^[9]
Synoptic Terrain Photography: To obtain high-quality photographs for research in geology, geophysics, geography, oceanography, and related fields.
Synoptic Weather Photography: To obtain selective high-quality photographs of clouds to study the fine structure of the Earth's weather system.
Nuclear Emulsion: To study the cosmic radiation incident on the Earth's atmosphere, to obtain detailed chemical composition of the heavy primary nuclei, and to search for rare particles.
Airglow Horizon Photography: To measure by direct photography the heights at which atomic oxygen and sodium layers occur in the upper atmosphere.
Ultraviolet Astronomical Camera: To test the techniques of ultraviolet photography under vacuum conditions and to obtain ultraviolet radiation observations of stars in wavelength region of 2,000 to 4,000 angstroms by spectral means.
Ion Wake Measurement: To determine and measure the ion and electron wake structure and perturbation of the ambient medium produced by an orbiting vehicle, and to study the changes in the ion flux and wake caused by thruster firings.
Earth-Moon Libration Region Photography: To investigate the regions of the L4 and L5 libration points of the Earth–Moon system to determine the possible existence of clouds of particulate matter orbiting the Earth in these regions.
Dim-Light Photography and Orthicon: To obtain photographs of various faint and diffuse astronomical phenomena.

Reentry[edit]

The mission ended with the first totally automatic, computer-controlled reentry by the U.S., which brought Gemini 11 down 2.8 miles (4.5 km) from its recovery ship USS Guam, only 1.5 miles (2.4 km) from the planned position.^[4]

Astronaut recovery was done by Navy Helicopter Squadron HS-3.

The Gemini 11 mission was supported by 9,054 United States Department of Defense personnel, 73 aircraft, and 13 ships.^[10]

Insignia[edit]

Since Conrad and Gordon were both members of the US Navy, the embroidered mission patch was designed in Navy colors: blue and gold. Stars are used to mark the major milestones of the mission. The first orbit Agena rendezvous is marked by a small gold star just above the Earth, to the left. The Agena docking is marked by a large star on the left. The star at the top marks the record high apogee reached by Gemini 11. Note that the scale is greatly exaggerated; their maximum altitude of 850 miles (1,370 km) is roughly the distance from St. Louis to Cape Kennedy. Finally, the star on the right marks Dick Gordon's spacewalk. The docking, record apogee and spacewalk are also shown on the patch by the Agena, orbital apogee path and spacewalking astronaut.

Potential lunar missions[edit]

Gemini 11's record altitude was ultimately the result of an internal race to the Moon. As early as 1961, NASA's Jim Chamberlin and McDonnell Aircraft had advocated using Gemini spacecraft to get to the Moon sooner than Apollo. Their proposals considered using Centaur rockets to boost the Gemini on a circumlunar trajectory (similar to the Soviet's Zond program), lunar orbit missions using Centaur rockets for translunar injection and Agena for lunar orbit insertion, and even lunar landing missions using Gemini in place of the Apollo Command Module and a small open-cockpit Langley Light LM in place of the Apollo Lunar Module. Multiple Titan or Saturn IB rockets, and even the abandoned Saturn C-3 were considered as the launch vehicles.

Pete Conrad liked these ideas and together with McDonnell corporations strongly advocated his Gemini 11 to be circumlunar. Discretely called 'Gemini - Large Earth Orbit', the plan would use a Titan IIIC-launched Transtage. The Gemini 11 crew would be launched with the Titan II GLV as they did in reality, and would dock with the Transtage, which would then boost them to translunar velocity. Conrad managed to stir Congressional interest, but NASA administrator James Webb informed them that any extra funds Congress cared to appropriate for such a project would be better spent accelerating the Apollo program. After further internal struggles, Conrad finally got NASA approval for the Agena on his Gemini 11 flight to boost him onto two record highly elliptical 1,370 km orbits. This high flight was the only remnant of lunar Gemini.^[11]

Spacecraft location[edit]

The Gemini 11 capsule on display at the California Science Center in Los Angeles

The spacecraft is on display at the California Science Center in Los Angeles, California.

Notes[edit]

This article incorporates public domain material from websites or documents of the National Aeronautics and Space Administration.

^ McDowell, Jonathan. "SATCAT". Jonathan's Space Pages. Retrieved March 23, 2014.
^ Hacker, Barton C.; Grimwood, James M. (September 1974). "Chapter 11 Pillars of Confidence". On the Shoulders of Titans: A History of Project Gemini. NASA History Series. Vol. SP-4203. NASA. p. 239. Archived from the original on 2010-01-13. Retrieved 2013-09-26. With Gemini IV, NASA changed to Roman numerals for Gemini mission designations.
^ Dumoulin, Jim (August 25, 2000), NASA Project Gemini-XI, archived from the original on February 1, 2012, retrieved April 12, 2010
^ ^a ^b ^c ^d ^e ^f ^g Gatland, Kenneth (1976), Manned Spacecraft, Second Revision, New York, NY, USA: MacMillan Publishing Co., Inc, pp. 180–182, ISBN 0-02-542820-9
^ Agle, D. C. (September 1998). "Flying the Gusmobile". Air & Space.
^ However, if Apollo had progressed as planned, the record would have been broken by what was designated as the E mission, which was a medium Earth orbital test of the complete Apollo spacecraft, with an apogee of 3,500 nautical miles (6,500 km) planned to be flown in March 1969. But the first Lunar Module was not ready in time for the D mission planned for December 1968, which was a low Earth orbit test (see List of Apollo missions). Therefore, the E mission was cancelled and replaced with the D mission in March, and Gemini 11's apogee record stands.
^ @spacex (15 September 2021). "Second phasing burn complete. Dragon and the @inspiration4x crew have reached a circular orbit of 585km – a new Dragon altitude record" (Tweet) – via Twitter.
^ "NASA Gemini 11 Press Kit" (PDF). Archived from the original (PDF) on 21 July 2011. Retrieved 2011-02-10.
^ Bender, M. A.; et al. (September 1971). "Radiation and zero-gravity effects on human leukocytes and Neurospora crassa". Nasa. Manned Spacecraft Center the Gemini Program Biomed. Sci. Expt. Sum. NASA. Archived from the original on 22 January 2017. Retrieved 22 January 2017.
^ Hacker, Barton C.; Grimwood, James M. (1977). "Appendix G DoD Support". On the Shoulders of Titans - The History of Project Gemini (PDF). p. 596. Retrieved December 18, 2022.
^ "Gemini: Lunar Gemini". Archived from the original on July 13, 2016.

External links[edit]

NASA Gemini 11 press kit - Sep 2, 1966
The short film Gemini XI is available for free viewing and download at the Internet Archive.
Spaceflight Mission Patches
NASA Space Science Data Coordinated Archive
U.S. Space Objects Registry

Preceded by Gemini 10 crew	Human altitude record 1966-1968	Succeeded by Apollo 8 crew

[satcat-1] McDowell, Jonathan. "SATCAT". Jonathan's Space Pages. Retrieved March 23, 2014.

[titans-2] Hacker, Barton C.; Grimwood, James M. (September 1974). "Chapter 11 Pillars of Confidence". On the Shoulders of Titans: A History of Project Gemini. NASA History Series. Vol. SP-4203. NASA. p. 239. Archived from the original on 2010-01-13. Retrieved 2013-09-26. With Gemini IV, NASA changed to Roman numerals for Gemini mission designations.

[3] Dumoulin, Jim (August 25, 2000), NASA Project Gemini-XI, archived from the original on February 1, 2012, retrieved April 12, 2010

[Gatland-4] ^ ^a ^b ^c ^d ^e ^f ^g Gatland, Kenneth (1976), Manned Spacecraft, Second Revision, New York, NY, USA: MacMillan Publishing Co., Inc, pp. 180–182, ISBN 0-02-542820-9

[agle199809-5] Agle, D. C. (September 1998). "Flying the Gusmobile". Air & Space.

[6] However, if Apollo had progressed as planned, the record would have been broken by what was designated as the E mission, which was a medium Earth orbital test of the complete Apollo spacecraft, with an apogee of 3,500 nautical miles (6,500 km) planned to be flown in March 1969. But the first Lunar Module was not ready in time for the D mission planned for December 1968, which was a low Earth orbit test (see List of Apollo missions). Therefore, the E mission was cancelled and replaced with the D mission in March, and Gemini 11's apogee record stands.

[7] @spacex (15 September 2021). "Second phasing burn complete. Dragon and the @inspiration4x crew have reached a circular orbit of 585km – a new Dragon altitude record" (Tweet) – via Twitter.

[8] "NASA Gemini 11 Press Kit" (PDF). Archived from the original (PDF) on 21 July 2011. Retrieved 2011-02-10.

[9] Bender, M. A.; et al. (September 1971). "Radiation and zero-gravity effects on human leukocytes and Neurospora crassa". Nasa. Manned Spacecraft Center the Gemini Program Biomed. Sci. Expt. Sum. NASA. Archived from the original on 22 January 2017. Retrieved 22 January 2017.

[10] Hacker, Barton C.; Grimwood, James M. (1977). "Appendix G DoD Support". On the Shoulders of Titans - The History of Project Gemini (PDF). p. 596. Retrieved December 18, 2022.

[11] "Gemini: Lunar Gemini". Archived from the original on July 13, 2016.

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v t e ← 1965 · Orbital launches in 1966 · 1967 →
January	Kosmos 104 OPS 2394 OPS 7253 OPS 3179 Kosmos 105 Kosmos 106 OPS 1593 Luna 9
February	OPS 7291 ESSA-1 OPS 1439 Kosmos 107 Kosmos 108 OPS 1184 OPS 3011 OPS 3031 Dipason Kosmos 109 DS-K-40 No.2 Kosmos 110 ESSA-2
March	Kosmos 111 OPS 3488 GATV-5003 Gemini VIII Kosmos 112 OPS 0879 OPS 0974 Kosmos 113 N-4 No.3 OPS 1117 Molniya-1 No.5 OV1-4 OV1-5 OPS 0340 Luna 10
April	Kosmos 114 OPS 1612 Surveyor SD-3 OAO-1 OPS 0910 Kosmos 115 OV3-1 Molniya 1-03 Kosmos 116
May	OPS 1508 Kosmos 117 Kosmos 118 OPS 1950 OPS 6785 Nimbus 2 Zenit-4 GATV-5004 OPS 0082 OPS 1788 Kosmos 119 Explorer 32 Surveyor 1
June	ATDA Gemini IX-A OPS 1577 OPS 1856 OGO-3 Kosmos 120 OV3-4 FTV-1351 Secor 6 ERS-16 OPS 9311 OPS 9312 OPS 9313 OPS 9314 OPS 9315 OPS 9316 OPS 9317 GGTS Kosmos 121 OPS 1599 PAGEOS Kosmos 122
July	Explorer 33 AS-203 Proton 3 Kosmos 123 OPS 1850 OV1-7 OV1-8 Kosmos 124 GATV-5005 Gemini X Kosmos 125 Kosmos 126 OPS 3014
August	OV3-3 Kosmos 127 OPS 1545 Lunar Orbiter 1 OPS 1832 OPS 6810 Pioneer 7 OPS 2366 FTV-1352 Secor 7 ERS-15 Luna 11 IDSCP 1 IDSCP 2 IDSCP 3 IDSCP 4 IDSCP 5 IDSCP 6 IDSCP 7 GGTS Kosmos 128
September	GATV-5006 Gemini XI OPS 6026 OPS 1686 OPS 6874 Zenit-2 No.40 OPS 6026 OPS 1686 OPS 6874 OGCh No.05L Surveyor 2 OPS 1703 Ōsumi 1 OPS 4096
October	ESSA-3 FTV-1583 Secor 8 OPS 2055 OPS 5345 Kosmos 129 Molniya 1-04 Kosmos 130 Luna 12 Surveyor SM-3 Intelsat II F-1 OV3-2
November	OGCh No.06L OPS 2070 OPS 5424 OPS 0855 OV4-1R OV4-1T OV1-6 Lunar Orbiter 2 OPS 1866 GATV-5001A Gemini XII Kosmos 131 Strela-2 No.1 Kosmos 132 Kosmos 133
December	Kosmos 134 OPS 1890 ATS-1 OV1-9 OV1-10 Kosmos 135 Soyuz 7K-OK No.1 OPS 8968 Biosatellite 1 Kosmos 136 Ōsumi 2 Kosmos 137 Luna 13 OPS 1584
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). Cubesats are smaller. Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).