Accession Number : AD0851201

Title :   Flight Proofing Test Report for Abort Sensing and Control Unit Drawing No. 27-11111-821,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Galloway, R. N. ; Denneny, F. J.

Report Date : 30 MAR 1961

Pagination or Media Count : 63

Abstract : 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)

Descriptors :   (*SURFACE TO SURFACE MISSILES, ABORT), DETECTORS, CONTROL SYSTEMS, TEST METHODS, HUMIDITY, THERMAL STRESSES, VIBRATION, ACCELERATION, PRESSURE SWITCHES, GYRO STABILIZERS, ELECTRICAL PROPERTIES, MANNED SPACECRAFT.

Subject Categories : Electrical and Electronic Equipment
      Mfg & Industrial Eng & Control of Product Sys

Distribution Statement : APPROVED FOR PUBLIC RELEASE