Gemini 11

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Gemini XI
Gemini XI conducting a tether experiment using the Agena Target Vehicle
Mission type
OperatorNASA
COSPAR ID1966-081A Edit this at Wikidata
SATCAT no.2415
Mission duration2 days 23 hours 17 minutes 9 seconds
Orbits completed44
Spacecraft properties
Spacecraft
McDonnell
Launch mass3,798 kilograms (8,374 lb)
Landing mass1,920 kilograms (4,230 lb)
Crew
Crew size2
Members
  • EVA
    duration
2 hours 41 minutes
Start of mission
Launch dateSeptember 12, 1966, 14:42:26 (1966-09-12UTC14:42:26Z) UTC
Rocket
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 11 (officially Gemini XI)

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

  • Perform a direct-ascent
    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 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 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

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

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

Fliteline Medallion

Since Conrad and Gordon were both members of the

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

Gemini 11's record altitude was ultimately the result of an internal race to

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

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

Los Angeles, California
.

See also

Notes

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.
  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
  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. 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 (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.
  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.

External links

Wikimedia Commons has media related to Gemini 11.
Preceded by Human altitude record
1966-1968 		Succeeded by
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