Centaur Fill and Drain Valve Flow and Pressure Drop Tests,

Abstract

This report defines tests performed to determine flow rate versus pressure drop across the Centaur liquid oxygen and liquid hydrogen fill and drain Valves 57-23209 while simulating missile environmental conditions. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 12, 1961
Accession Number
AD0844843

Entities

People

  • J. E. Frink

Organizations

  • General Dynamics

Tags

DTIC Thesaurus Topics

  • Cryogenic Propellants
  • Drop Tests
  • Energetic Materials
  • Flow Rate
  • Hydrogen
  • Liquid Hydrogen
  • Liquid Oxygen
  • Liquid Propellants
  • Liquid Rocket Propellants
  • Materials
  • Propellants

Readers

  • Aerospace Engineering
  • Combustion science or combustion engineering.
  • Electrical Engineering