Accession Number : AD0842588

Title :   'E' Series LO2 System Surge Suppression Study.

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Adams, P. C.

Report Date : 18 NOV 1960

Pagination or Media Count : 28

Abstract : High surge pressures occur at the 'E' Series turbopump inlet prior to engine start. Two methods of reducing these surges were evaluated; Helium injection, and Surge Chambers near the turbopump inlet. (Author)

Descriptors :   *LIQUID ROCKET PROPELLANTS), *PRESSURE REGULATORS), (*SURFACE TO SURFACE MISSILES, (*TURBOPUMPS, LIQUID ROCKET OXIDIZERS, PRESSURE, HIGH PRESSURE VALVES, CALIBRATION, HELIUM.

Subject Categories : Pumps, Filters, Pipes, Tubing, Fittings & Vlvs
      Test Facilities, Equipment and Methods
      Surface-launched Guided Missiles

Distribution Statement : APPROVED FOR PUBLIC RELEASE