PREIGNITION PRODUCTS FROM STORABLE PROPELLANTS AT SIMULATED HIGH-ALTITUDE CONDITIONS

Abstract

In view of the destructive ignitions that occur in hypergolic test firings of attitude-control motors under simulated high-altitude conditions, the preignition behavior of MMH, UDMH, A-50, and N2H4 with N2O4 was examined at low pressures and temperatures in the laboratory.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1967
Accession Number
AD0665884

Entities

People

  • David W Taylor
  • Leroy Schieler
  • Stanley W. Mayer

Organizations

  • The Aerospace Corporation

Tags

Communities of Interest

  • Sensors
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Absorption Spectra
  • Chemical Reactions
  • Combustion
  • Combustion Chambers
  • Differential Thermal Analysis
  • Exothermic Reactions
  • Explosives
  • High Altitude
  • Ignition Lag
  • Low Temperature
  • Material Degradation Processes
  • Materials
  • Materials Laboratories
  • Measurement
  • Propellants
  • Rocket Oxidizers
  • Thermal Analysis

Fields of Study

  • Physics

Readers

  • Astronomy and Astrophysics.
  • Combustion science or combustion engineering.
  • Explosive Engineering.