Steady State Analysis of Hydrazine Catalytic Thrusters for Different Types of Catalysts

Abstract

A theoretical analysis has been made to determine the characteristics of the steady state behaviour of a hydrazine decomposition engine. The model makes use of the simplification that consists in considering that the ammonia decomposition is only important at high temperatures. The results are valid for different types of catalysts with different stoichiometries and reaction rates for hydrazine and ammonia decomposition. Conditions at the chamber exit are obtained analytically as a function of chamber length and other characteristics, in particular expressions are given for fractional ammonia decomposition at the exit and the specific impulse obtained if the outgoing mixture would be expanded to the vacuum. Fluid and particle temperature distributions along the chamber are also calculated keeping, however, fixed a non-dimensional parameter expressing the ratio of the mass and heat transfer from the interstitial fluid to the particle.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jan 15, 1976
Accession Number
ADA023231

Entities

People

  • Antonio Crespo

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Catalytic Reactors
  • Computer Programs
  • Differential Equations
  • Engines
  • Equations
  • Flow Rate
  • Heat Transfer
  • High Temperature
  • Hydrogen
  • Mass Flow
  • Nitrogen Compounds
  • Scientific Research
  • Specific Impulse
  • Surface Properties
  • Surface Temperature
  • Thrusters

Readers

  • Calculus or Mathematical Analysis
  • Combustion and Flow Dynamics.
  • Combustion science or combustion engineering.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster