The purpose of the report is to describe the test equipment and procedure required for the flight proofing of components of a 'square canister' containing six rate gyro output detectors, thirteen pressure switch output detectors and associated circuitry needed to supply two 'ready-abort' outputs as well as seventeen telemetry outputs. (Author)
Flight Proofing Test Report for Abort Sensing and Control Unit Drawing No. 27-11111-821
1961
63 pages
Report
Keine Angabe
Englisch
Resistive, Capacitive, & Inductive Components , Quality Control & Reliability , Surface to surface missiles , Abort , Detectors , Control systems , Test methods , Humidity , Thermal stresses , Vibration , Acceleration , Pressure switches , Gyro stabilizers , Electrical properties , Manned spacecraft
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