The purpose of the report is to describe the test equipment and procedure required for the flight proofing of six rate gyro output detectors.
Flight Proofing Test Report for Abort Sensing and Control Unit-Mercury-Missileborne Dwg. No. 27-11111-1
1960
70 pages
Report
Keine Angabe
Englisch
Navigation, Guidance, & Control , Space Launch Vehicles & Support Equipment , Launch vehicles , Stabilization systems , Abort , Detectors , Ejection , Manned spacecraft , Spaceborne , Control systems , High altitude , Humidity , Vibration , Acceleration , Thermal stability , Capacitors , Diodes , Failure , Pressure switches , Electrical properties , Atlas launch vehicles , Mercury project