Gemini 11

Crew

Backup crew

Support crew

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

Mission parameters

• Mass: 8374 lb

Highest orbit (followed twice):

• Perigee: 298 km
• Apogee: 1374 km
• Inclination: 28.85°
• Period: 101.52 min

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: 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 and 8 minutes

Objectives

• 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.
• Perform miscellaneous scientific experiments.
• Perform a computer-controlled atmospheric reentry to a precision splashdown point.

Flight

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.

Gemini 11 used the rocket on its Agena target vehicle to raise its apogee to 853 mi, the highest Earth orbit ever reached by a crewed spacecraft at the time. The perigee was 179 mi, and maximum velocity (at perigee) was 17967 mph.

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 mi.

Gordon's first EVA, planned to last for two hours, involved fastening a 100 ft 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 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 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. 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.

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.

Scientific experiments

The 12 scientific experiments were:

• 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.
• 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 (Kordylewski clouds).
• 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 mi from its recovery ship USS Guam, only 1.5 mi from the planned position.

Astronaut recovery was done by United States Navy Helicopter Anti-Submarine Squadron 3.

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

Insignia

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 mi 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

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.

Spacecraft location

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

Notes

References

References

1. McDowell, Jonathan. "SATCAT". Jonathan's Space Pages.
2. Hacker, Barton C.. (September 1974). "On the Shoulders of Titans: A History of Project Gemini". NASA.
3. Dumoulin, Jim. (August 25, 2000). "NASA Project Gemini-XI".
4. McDowell, Jonathan. (September 11, 2024). "For comparison, the best data I have for Gemini 11 suggests an apogee of 1374.0 km (standard height) with a geoid height maxium of 1377.9 km. However this is not an SGP4 dataset and perturbations are not taken into account – could be 2 km off. Clear that Polaris Dawn was higher.".
5. Gatland, Kenneth. (1976). "Manned Spacecraft, Second Revision". MacMillan Publishing Company, Incorporated.
6. Agle, D. C.. (September 1998). "Flying the Gusmobile".
7. (15 September 2021). "Second phasing burn complete. Dragon and the @inspiration4x crew have reached a circular orbit of 585km – a new Dragon altitude record".
8. "NASA Gemini 11 Press Kit".
9. Bender, M. A.. (September 1971). "Radiation and zero-gravity effects on human leukocytes and Neurospora crassa". NASA.
10. Hacker, Barton C.. (1977). "On the Shoulders of Titans – The History of Project Gemini".
11. "Gemini: Lunar Gemini".