A Mechanistic Study of Nitromethane Decomposition on Ni Catalysts.

Abstract

Nitromethane is one of several compounds which decomposes exothermically and may be used as a monopropellant in small rocket thrusters and demand gas generators. The use of nitromethane for such uses has not received much attention due to the absence of an appropriate catalyst to facilitate its decomposition. Recently, the decomposition of nitromethane over Ni0 and Cr203 catalysts has been examined to examine the feasibility of a nitro-methane-based monopropellant system. These studies indicated that a Ni0/alumina catalyst was effective in causing nitromethane decomposition. However, relative to existing hydrazine based monopropellant systems the nitromethane-Ni0/alumina system suffered two severe drawbacks; first, it required much higher light-off temperatures than hydrazine based systems, and second, the decomposition reaction poisoned the catalyst with carbon degrading performance with continued use.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1982
Accession Number
ADA128444

Entities

People

  • Jay Benziger

Organizations

  • Princeton University

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Auger Electron Spectroscopy
  • Auger Electrons
  • Catalysts
  • Chemical Reactions
  • Electron Spectroscopy
  • Engineering
  • Heat Of Activation
  • Hydrazines
  • Kinetics
  • Materials
  • Methanes
  • Monopropellants
  • Oxidation
  • Poisoning
  • Propellants
  • Spectra
  • Spectrometry

Readers

  • Rocket Propulsion.
  • Surface Engineering/Surface Coating Technology.
  • Systems Analysis and Design

Technology Areas

  • Space
  • Space - Hall-Effect Thruster