Accession Number : AD0830945

Title :   'D' SERIES (PN) 7-43040 ALIGNMENT PROCEDURE (FUEL/LO2 RATIO VALVE).

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Report Date : 14 MAR 1959

Pagination or Media Count : 8

Abstract : The field test procedure is designed to be used in the alignment of the propellant utilization valve with the missile in the vertical position. (Author)

Descriptors :   (*SURFACE TO SURFACE MISSILES, PROPELLANT CONTROL), (*HYDRAULIC VALVES, ALIGNMENT), MODEL TESTS, LIQUID PROPELLANT ROCKET ENGINES, LAUNCHING SITES, TEST METHODS, SEQUENCES(MATHEMATICS), TEST EQUIPMENT, GUIDED MISSILE PERSONNEL, LIQUID ROCKET OXIDIZERS, INSTRUCTION MANUALS, SUSTAINER ENGINES, IGNITION, CHECKOUT PROCEDURES.

Subject Categories : Pumps, Filters, Pipes, Tubing, Fittings & Vlvs
      Surface-launched Guided Missiles
      Liquid Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE