Accession Number : AD0833165

Title :   SUSTAINER LIQUID OXYGEN LINE PRESSURE LOSS TEST,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Maderazo, B.

Report Date : 07 AUG 1959

Pagination or Media Count : 26

Abstract : The purpose of testing was to determine the pressure loss of a redesigned liquid oxygen sustainer line and to investigate the flow characteristics of a redesigned liquid oxygen sustainer line. (Author)

Descriptors :   (*SUSTAINER ENGINES, PROPELLANT CONTROL), (*PIPES, PRESSURIZATION), LIQUID ROCKET OXIDIZERS, SURFACE TO SURFACE MISSILES, PRESSURE, ATTRITION, MODIFICATION KITS, CHECKOUT PROCEDURES, SEQUENCES(MATHEMATICS), TEST EQUIPMENT, OXYGEN, FLUID FLOW, VELOCITY, TABLES(DATA).

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

Distribution Statement : APPROVED FOR PUBLIC RELEASE