Accession Number : AD0830225

Title :   FUEL TANK PRESSURIZATION 'B' CONFIGURATION,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Kuhlman, D. W.

Report Date : 24 NOV 1958

Pagination or Media Count : 7

Abstract : The object of this test was to operationally check the airborne fuel tank pressurization system under the simulated booster condition, that exists just prior to and at booster separation. (Author)

Descriptors :   *PROPELLANT TANKS), (*SURFACE TO SURFACE MISSILES, PRESSURIZATION, SIMULATION, STAGING, SAFETY VALVES, MODEL TESTS, HELIUM, PERFORMANCE(ENGINEERING), TEST METHODS.

Subject Categories : Surface-launched Guided Missiles
      Liquid Propellant Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE