Accession Number : AD0830925

Title :   SM-65D PROPELLANT UTILIZATION SYSTEM CHECKOUT DESCRIPTION AND PLAN FOR ACOUSTICA ASSOCIATES, INC., MODEL PU-100, PUL-130 AND PUL-132,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Loukes, L. F.

Report Date : 08 APR 1959

Pagination or Media Count : 16

Abstract : The document establishes the test objectives required to perform a complete systems test level checkout of the Model PU-100, PUL-130, PUL 132 missileborne propellant utilization system for factory checkout or assembly building area. The document also describes the method by which the parameters are measured and the capabilities required of the checkout equipment. (Author)

Descriptors :   (*SURFACE TO SURFACE MISSILES, LIQUID PROPELLANT ROCKET ENGINES), (*PROPELLANT CONTROL, CHECKOUT PROCEDURES), LIQUID ROCKET PROPELLANTS, LIQUID ROCKET OXIDIZERS, PROPELLANT TRANSFER, DETECTORS, TRANSDUCERS, CHECKOUT EQUIPMENT, TEST METHODS, SEQUENCES(MATHEMATICS), ELECTRICAL IMPEDANCE, FEEDBACK, GUIDED MISSILE COMPUTERS.

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

Distribution Statement : APPROVED FOR PUBLIC RELEASE