Accession Number : AD0843171

Title :   Centaur Propellant Utilization Ratio Error Detector Assembly. Vibration Test Procedure.

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Lanterman, B. A.

Report Date : 28 FEB 1962

Pagination or Media Count : 9

Abstract : The purpose was to specify requirements and procedures for testing and checkout of the Centaur ratio error detector assembly during vibration. (Author)

Descriptors :   (*LAUNCH VEHICLES, PROPELLANT CONTROL), (*PROPELLANT CONTROL, DETECTORS), ERRORS, RELIABILITY, ENVIRONMENTAL TESTS, VIBRATION, CHECKOUT PROCEDURES.

Subject Categories : Liquid Rocket Propellants
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Distribution Statement : APPROVED FOR PUBLIC RELEASE