Accession Number : AD0842762

Title :   Flight Proofing Test Report for Abort Sensing and Control Unit-Mercury-Missileborne Dwg. No. 27-11111-1.

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Smith, R. J.

Report Date : 05 AUG 1960

Pagination or Media Count : 70

Abstract : The purpose of the report is to describe the test equipment and procedure required for the flight proofing of six rate gyro output detectors.

Descriptors :   (*LAUNCH VEHICLES, ABORT), (*STABILIZATION SYSTEMS, DETECTORS), EJECTION, MANNED SPACECRAFT, SPACEBORNE, CONTROL SYSTEMS, HIGH ALTITUDE, HUMIDITY, VIBRATION, ACCELERATION, THERMAL STABILITY, CAPACITORS, DIODES, FAILURE, PRESSURE SWITCHES, ELECTRICAL PROPERTIES.

Subject Categories : Ground Support Sys & Facil For Space Vehicles

Distribution Statement : APPROVED FOR PUBLIC RELEASE