The objective of the test is to demonstrate that the personnel recovery and survival equipment system conforms with astronautics drawings under conditions simulating those existing, after seat-man separation following emergency ejection. (Author)
Gemini B Ejection Seat Functional Test Air Drop Test Plan
1967
16 pages
Report
No indication
English
Industrial Safety Engineering , Manned Spacecraft , Manned spacecraft , Ejection seats , Space stations , Drop tests , Space capsules , Packs(Parachute) , Survival kits , Redundant components , Automatic , Explosive actuators , Pressure suits , Aerospace systems , Escape systems , Disconnect fittings , Test methods , Safety , Space crews , Gemini b project , Manned orbiting laboratories , Mol(Manned orbiting laboratories) , Gemini
Gemini B Structural Qualification Test Plan
NTIS | 1968
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NTIS | 1969