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Gemini 11

Gemini XI
Gemini 11 Agena.jpg
Gemini XI conducting a tether experiment using the Agena Target Vehicle
Operator NASA
COSPAR ID 1966-081A
SATCAT № 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
Start of mission
Launch date September 12, 1966, 14:42:26 (1966-09-12UTC14:42:26Z) 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 (1966-09-15UTC13:59:36Z) UTC
Landing site 24°15.4′N 70°0′W / 24.2567°N 70.000°W / 24.2567; -70.000 (Gemini 11 splashdown)
Orbital parameters
Reference system Geocentric
Regime Low Earth orbit
Perigee 298 kilometers (161 nmi)
Apogee 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

Gemini 11 patch.png

Gemini 11 prime crew (Gordon and Conrad).jpg
(Left to Right) Gordon & Conrad
← Gemini 10
Gemini 12 →

Gemini 11 patch.png

Gemini 11 (officially Gemini XI)) was the ninth manned spaceflight mission of NASA's Project Gemini, which flew from September 12 to 15, 1966. It was the 17th manned 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 one hour and thirty-four 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 and 41 minutes.

Highest orbit (followed twice):

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 850 miles (1,370 km), the highest Earth orbit ever reached by a manned spacecraft. The perigee was 179 miles (288 km), and maximum velocity (at perigee) was 17,967 miles per hour (28,915 km/h). The apogee record stands as of March 2016, even though men have achieved greater distances from Earth by flying to the Moon in the Apollo program. The maximum operational altitude of the Space Shuttle was lower, at 600 miles (970 km).


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