The Ejection Seat Functional Test Fixture is used to support the spacecraft seat and simulate flight loads for checkout of the harness release mechanism. It also provides checkout of the seat/man separator. The purpose of the Space Technical Data Report (STDR) is to familiarize personnel with the operation and service of the Ejection Seat Functional Test Fixture. The report presents a description of the test fixture, its controls and functions and servicing instructions for preventive maintenance. (Author)
Operation and Service Manual for Ejection Seat Functional Test Fixture 52E040089
1967
35 pages
Report
Keine Angabe
Englisch
Industrial Safety Engineering , Manned Spacecraft , Manned spacecraft , Space stations , Aerospace systems , Ejection seats , Instruction manuals , Space capsules , Spacecraft seats , Safety belts , Release mechanisms , Loads(Forces) , Maintenance , Calibration , Gemini b project , Manned orbiting laboratories , Mol(Manned orbiting laboratories) , Gemini
Rocket ejection seat primary power ejection test system
Europäisches Patentamt | 2024
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