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Also known as Gemini IX-A, Gemini 9AもしくはGemini IX-A

crewed spaceflight in NASA's Gemini program

Key facts

Mission type
Space rendezvous Spacecraft docking (failed) Extravehicular activity
Operator
NASA
Cospar id
1966-047A
Mission duration
3 days, 20 minutes, 50 seconds
Spacecraft
Gemini SC9
Manufacturer
McDonnell
Launch mass
3,800 kilograms (8,300 lb)
Members
Thomas P. Stafford Eugene A. Cernan
Eva duration
2 hours, 7 minutes
Launch date
June 3, 1966, 13:39:33 ( 1966-06-03UTC13:39:33Z ) UTC
Rocket
Titan II GLV , s/n #62-12564
Launch site
Cape Kennedy LC-19
Recovered by
USS Wasp
Landing date
June 6, 1966, 14:00:23 ( 1966-06-06UTC14:00:24Z ) UTC
Landing site
27°52′N 75°0′W / 27.867°N 75.000°W / 27.867; -75.000
Reference system
Geocentric
Regime
Low Earth orbit
Perigee altitude
272 kilometers (147 nmi)

via Wikipedia infobox

Wikidata facts

Duration
260450
Mass
3750
Orbital period
89.97
Image
The Actual Gemini 9 Prime Crew - GPN-2000-001353.jpg
Show 7 more facts
Commons category
Gemini 9
UTC date of spacecraft launch
1966-06-03
orbits completed
47
UTC date of spacecraft landing
1966-06-06
apoapsis
274
periapsis
272
orbital inclination
28.8
Sources (2)

via Wikidata · CC0

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Article

Gemini 9A (officially Gemini IX-A) was a 1966 crewed spaceflight in NASA's Gemini program. It was the seventh crewed Gemini flight, the 15th crewed American flight and the 23rd spaceflight of all time (includes X-15 flights over 100 kilometers (62 mi; 54 nmi)). The original crew for Gemini 9, command pilot Elliot See and pilot Charles Bassett, were killed in a crash on February 28, 1966, while flying a T-38 jet trainer to the McDonnell Aircraft plant in St. Louis, Missouri to inspect their spacecraft. Their deaths promoted the backup crew, Thomas P. Stafford and Eugene Cernan, to the prime crew. The mission was renamed Gemini 9A after the original May 17 launch was scrubbed when the mission's Agena Target Vehicle was destroyed after a launch failure. The mission was flown June 3–6, 1966, after launch of the backup Augmented Target Docking Adaptor (ATDA). Stafford and Cernan rendezvoused with the ATDA, but were unable to dock with it because the nose fairing had failed to eject from the docking target due to a launch preparation error. Cernan performed a two-hour extravehicular activity, during which it was planned for him to demonstrate free flight in a self-contained rocket pack, the USAF Astronaut Maneuvering Unit. He was unable to accomplish this due to stress, fatigue, and overheating.

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