Solid Propellant Hydrogen Generator.

Abstract

Solid reactant hydrogen gas generator formulations which yield greater than 15 weight percent hydrogen of greater than 98 mole percent hydrogen of greater than 98 mole percent hydrogen purity are formulated of a primary heat and hydrogen source selected from ammonia borane from about 50 to about 70 weight percent and hydrazine bisborane from about 0-30.00 weight percent, a first hydrogen-containing compound that functions as an auxiliary heat and hydrogen source consisting of ammonium nitrate from about 10.20 to about 17.82 weight percent, and a second hydrogen-containing compound that functions as an auxiliary heat and hydrogen source consisting of (NH4)2B10H10 from about 9.80 to about 17.18 weight percent. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 20, 1982
Accession Number
ADD010005

Entities

People

  • Glen D. Artz
  • Louis R. Grant

Organizations

  • United States Army

Tags

DTIC Thesaurus Topics

  • Ammonium Nitrate
  • Energetic Materials
  • Generators
  • Hydrazines
  • Hydrogen
  • Materials
  • Nitrates
  • Propellants
  • Rocket Oxidizers
  • Solid Propellants

Readers

  • Mathematics or Statistics
  • Organic Chemistry
  • Rocket Propulsion.