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accelerometer acceptance testing AIAA aircraft analysis Apollo Apollo Program Apollo spacecraft approach assembly avionics Biosatellite CALIFORNIA/APRIL 1-3 capability catastrophic failures centrifuge certification test checkout component configuration Cornell Aeronautical Laboratory cost CPFL cycle defects defined demonstration density determine distribution drift failure Dutch roll dynamic engineering environment environmental equation equipment error evaluation facilities factor failure rate flight control Flight Dynamics frequency function ground test gyro hardware initial input installation Integrated Test interface launch load magnetic tape matrix maximum measured ment method mission mode module monitoring NASA operational orbital output performance phase phugoid pilot prior problems publication rights reserved reliability repair reserved by American rocket samples schedule shown in Figure simulation SPACE STATION spacecraft specific structure Subroutine subsystem system test tape techniques temperature test data test planning test procedure test requirements test station tion V/STOL variables vehicle verification Weapon System