Accession Number : AD0829628

Title :   PROPELLANT UTILIZATION SYSTEM XSM-65B1 THRU B13 COMPONENTS TEST REQUIREMENTS,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Heironimus, P. E.

Report Date : 09 APR 1957

Pagination or Media Count : 22

Abstract : The requirements listed herein contain the important or vital Parameters deemed necessary to insure proper operation of the Assemblies, Sub-Assemblies and Components of the Propellant Utilization System. (Author)

Descriptors :   *PROPELLANT CONTROL), (*SURFACE TO SURFACE MISSILES, TEST METHODS, SEQUENCES(MATHEMATICS), CHECKOUT EQUIPMENT, CONTROL SYSTEMS, ELECTRONIC EQUIPMENT, LIQUID ROCKET OXIDIZERS, POWER SUPPLIES.

Subject Categories : Surface-launched Guided Missiles
      Liquid Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE