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Gemini 11

Summary

Gemini XI
Gemini 11 Agena.jpg
Gemini XI conducting a tether experiment using the Agena Target Vehicle
OperatorNASA
COSPAR ID1966-081A
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
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°15.4′N 70°0′W / 24.2567°N 70.000°W / 24.2567; -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
Gemini 11 patch.png Gemini 11 prime crew (Gordon and Conrad).jpg
Gordon (left) and Conrad 

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-ever 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 world-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

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

Backup crew

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

Support crew

Mission parameters

  • Mass: 8,374 pounds (3,798 kg)

Highest orbit (followed twice):

Docking

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

Space walk

  • 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

Gemini 11 launch
An Atlas 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

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 June 2020, 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 380 miles (610 km).

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

The 12 scientific experiments were:[7]

  • 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.[8]
  • 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

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.[citation needed]

Insignia

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. 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.

Spacecraft location

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 Center in Los Angeles, California.

See also

Notes

 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.
  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. SP-4203. NASA. p. 239. With Gemini IV, NASA changed to Roman numerals for Gemini mission designations.
  3. ^ Dumoulin, Jim (August 25, 2000), NASA Project Gemini-XI, retrieved April 12, 2010
  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
  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. ^ "NASA Gemini 11 Press Kit" (PDF). Archived from the original (PDF) on 21 July 2011. Retrieved 2011-02-10.
  8. ^ Bender, M. A.; et al. "Radiation and zero-gravity effects on human leukocytes and Neurospora crassa". NASA Technical Reports Server (NTRS). NASA. Archived from the original on 22 January 2017. Retrieved 22 January 2017.

External links

  • NASA Gemini 11 press kit - Sep 2, 1966
  • The short film Gemini XI is available for free download at the Internet Archive
  • Spaceflight Mission Patches
  • NASA Space Science Data Coordinated Archive
  • U.S. Space Objects Registry https://web.archive.org/web/20090521121750/http://usspaceobjectsregistry.state.gov/search/index.cfm