PROPERTIES OF MATERIALS AT LIQUID OXYGEN AND LIQUID HYDROGEN TEMPERATURES.

Abstract

This report is the result of a survey of the properties of materials at liquid oxygen (-293F) and liquid hydrogen (-423F) temperatures performed to assist in the selection of suitable materials for propellant tanks, bellows, and propellant lines in a satellite missile. (Author)

Document Details

Document Type
Technical Report
Publication Date
Mar 15, 1957
Accession Number
AD0676736

Entities

People

  • A. Hurlich

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Artificial Satellites
  • Energetic Materials
  • Hydrogen
  • Liquid Hydrogen
  • Liquid Oxygen
  • Liquid Propellants
  • Liquid Rocket Propellants
  • Materials
  • Propellant Tanks
  • Propellants
  • Rocket Propellants

Readers

  • Electrical Engineering
  • Rocket Propulsion.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster