Stability and Compatibility Studies on Advanced Rocket Propellant Components

Abstract

A number of candidate advanced propellant ingredients were studied with the objective of obtaining definitive information regarding their usefulness in new propellant systems. The research was laboratory based, involved small quantities (generally less than 100 mg.) of the ingredient, and dealt generally with the stability of individual ingredients and with stability- compatibility of two or more components of proposed propellants. The ingredients studied include: Perchlorates--HAP, HP-2, DOAP and AP (for comparison); N-F materials--P-BEP, TVOPA and P-722; Fuel--AlH3; and numerous state-of-the-art binder prepolymers and curatives.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1970
Accession Number
AD0511670

Entities

People

  • A. D. Mcelroy
  • Ivan C. Smith
  • John W. Nebgen
  • Raymond E. Foscante

Organizations

  • MRIGlobal

Tags

Communities of Interest

  • Advanced Electronics
  • Weapons Technologies

DTIC Thesaurus Topics

  • Alkenes
  • Chemical Reactants
  • Chemical Reaction Properties
  • Chemical Synthesis
  • Chemistry
  • Dielectric Gases
  • Ethers
  • Mass Spectrometry
  • Materials Science
  • Organic Chemistry
  • Spectra
  • Spectrometry
  • Spectroscopy

Fields of Study

  • Physics

Readers

  • Rocket Propulsion.
  • Theoretical Analysis.