Accession Number : AD0833245

Title :   SUSTAINER ENGINE CONTROL SYSTEM SHUTDOWN CHARACTERISTICS WITH HYDRAULIC FAILURE, WS107A,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Shannon, P. S.

Report Date : 12 SEP 1959

Pagination or Media Count : 12

Abstract : This test procedure corroborates the integrity of a liquid rocket sustainer engine hydraulic accumulator relative to control systems pressure decay.

Descriptors :   *HYDRAULIC EQUIPMENT), (*SURFACE TO SURFACE MISSILES, LIQUID PROPELLANT ROCKET ENGINES), (*SUSTAINER ENGINES, CONTROL SYSTEMS, PRESSURE, HYDRAULIC EQUIPMENT, FAILURE(MECHANICS), HYDRAULIC ACCUMULATORS, GROUND SUPPORT EQUIPMENT, CHECKOUT PROCEDURES.

Subject Categories : Surface-launched Guided Missiles
      Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE