Liquid Oxygen Pressure Loss Phase I and II,

Abstract

The pressure loss in the Centaur liquid oxygen system is a factor in the determination of the net positive suction head available to the turbopumps. The purpose of the tests is to determine the pressure loss in the Oxidizer Main Supply Duct (55-21504) while flowing liquid oxygen at various flow rates. (Author)

Document Details

Document Type
Technical Report
Publication Date
May 12, 1961
Accession Number
AD0843524

Entities

People

  • P. R. Laberge

Organizations

  • General Dynamics

Tags

DTIC Thesaurus Topics

  • Cryogenic Propellants
  • Energetic Materials
  • Flow Rate
  • Liquid Oxygen
  • Liquid Propellants
  • Liquid Rocket Propellants
  • Materials
  • Mechanisms (Engineering)
  • Turbopumps

Readers

  • Combustion and Flow Dynamics.
  • Rocket Propulsion.