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Contents

   



(Top)
 


1 Crew  



1.1  Backup crew  





1.2  Support crew  







2 Mission parameters  



2.1  Docking  





2.2  Space walk  







3 Objectives  





4 Flight  



4.1  Scientific experiments  





4.2  Reentry  







5 Insignia  





6 Potential lunar missions  





7 Spacecraft location  





8 See also  





9 Notes  





10 External links  














Gemini 11






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From Wikipedia, the free encyclopedia
 


Gemini XI
Gemini XI conducting a tether experiment using the Agena Target Vehicle
Mission type
  • Spacecraft docking
  • Extravehicular activity
  • OperatorNASA
    COSPAR ID1966-081A Edit this at Wikidata
    SATCAT no.2415
    Mission duration2 days 23 hours 17 minutes 9 seconds
    Orbits completed44
    Spacecraft properties
    SpacecraftGemini SC11
    ManufacturerMcDonnell
    Launch mass3,798 kilograms (8,374 lb)
    Landing mass1,920 kilograms (4,230 lb)
    Crew
    Crew size2
    Members
  • Richard F. Gordon Jr.
  • EVAs2
    EVA duration2 hours 41 minutes
    Start of mission
    Launch dateSeptember 12, 1966, 14:42:26 (1966-09-12UTC14:42:26Z) UTC
    RocketTitan II GLV
    Launch siteCape Kennedy LC-19
    End of mission
    Recovered byUSS Guam
    Landing dateSeptember 15, 1966, 13:59:35 (1966-09-15UTC13:59:36Z) UTC
    Landing site24°15′N 70°0′W / 24.250°N 70.000°W / 24.250; -70.000 (Gemini 11 splashdown)
    Orbital parameters
    Reference systemGeocentric
    RegimeLow Earth orbit
    Perigee altitude298 kilometers (161 nmi)
    Apogee altitude1,368 kilometers (739 nmi)
    Inclination28.8 degrees
    Period101.57 minutes
    EpochSeptember 14, 1966[1]
    Docking with GATV-5006
    Docking dateSeptember 12, 1966, 16:16:00 UTC
    Undocking dateSeptember 14, 1966, 16:55:00 UTC
    Time docked2 days 39 minutes

    Gordon (left) and Conrad
    ← 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]

    Mission parameters[edit]

    Highest orbit (followed twice):

    Docking[edit]

    Space walk[edit]

    Objectives[edit]

    Gemini 11 launch
    AnAtlas launch vehicle launches GATV-5006 into orbit for the Gemini 11 mission.
    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]

    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]

    Gemini 11 space-flown Fliteline Medallion

    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. LouistoCape 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]

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

    The spacecraft is on display at the California Science CenterinLos Angeles, California.

    See also[edit]

    Notes[edit]

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

    1. ^ 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 (September 16, 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]

    Preceded by

    Gemini 10 crew

    Human altitude record
    1966-1968
    Succeeded by

    Apollo 8 crew


    Retrieved from "https://en.wikipedia.org/w/index.php?title=Gemini_11&oldid=1154565858"

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