EXPERIMENTAL EVALUATION OF ADVANCED LIQUID PROPELLANTS.

Abstract

This report summarizes experimental propellant studies accomplished by the Evaluation and Test Branch, Propellant Division, AFRPL. The preparation and evaluation of 43% aluminum in hydrazine emulsion and the evaluation of alumizine 43G32 with nitrogen tetroxide are reported. The results of the evaluation of Hybaline B3 with nitrogen tetroxide are discussed. The evaluation of two water-cooled rocket engines is reported as are the plans for an altitude ignition delay tester. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1965
Accession Number
AD0367802

Entities

People

  • J. D. Willard
  • J. M. Hobbs
  • K. E. Nidiffer

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Altitude
  • Aluminum
  • Emulsions
  • Energetic Materials
  • Engines
  • Hydrazines
  • Ignition
  • Ignition Lag
  • Liquid Propellants
  • Materials
  • Nitrogen
  • Propellants
  • Rocket Engines
  • Rocket Oxidizers
  • Test And Evaluation
  • Tetroxides

Fields of Study

  • Physics

Readers

  • Rocket Propulsion.
  • Technical Research and Report Writing.