Development of a Low-Cost Catalyst for Hydrazine

Abstract

A low cost, active, highly stable hydrazine monopropellant decomposition catalyst has been developed. This catalyst utilizes ruthenium for its active component. Laboratory and thruster studies indicate that it is highly active at low ignition temperatures and shows unusually high resistance to loss of surface area during motor firing. A cobalt containing catalyst was also developed. This catalyst has lower activity for hydrazine decomposition at 5 deg C; however, it is active at higher temperatures and can be employed where short ignition delays at low temperature are not required and where extremely low cost is a desired property. Results of studies with various cobalt containing catalysts, cobalt-noble metal hybrid catalysts and ruthenium containing catalysts using several different substrate materials are also reported.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1970
Accession Number
AD0509420

Entities

People

  • Martin Lieberman
  • William F. Taylor

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Chemistry
  • Contracts
  • Heat Of Activation
  • High Temperature
  • Ignition Lag
  • Jet Propulsion
  • Low Temperature
  • Mass Transfer
  • Materials
  • Materials Science
  • Military Research
  • Rocket Engines
  • Rocket Propulsion
  • Three Dimensional
  • Transition Metals
  • Tungsten

Fields of Study

  • Chemistry

Readers

  • Aerospace Propulsion Engineering.
  • Electrochemical Engineering/ Fuel Cell Technologies

Technology Areas

  • Space
  • Space - Hall-Effect Thruster