Some Considerations Relating to Combustion in Rocket Motors

Abstract

An account is given of some of the problems associated with combustion in rocket motors and it is shown that the improvements in rocket motor performance which may result from a greater knowledge of the combustion process are considerable. Suggestions are made for tackling some of the problems involved.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1950
Accession Number
ADA474135

Entities

People

  • W. R. Maxwell

Organizations

  • Royal Aircraft Establishment

Tags

DTIC Thesaurus Topics

  • Chemical Reactions
  • Chemistry
  • Combustion
  • Combustion Chambers
  • Heat Transfer
  • Ignition
  • Liquid Phases
  • Liquid Propellants
  • Low Temperature
  • Materials Laboratories
  • Nitric Acid
  • Propellants
  • Rocket Engines
  • Rocket Oxidizers
  • Rocket Propellants
  • Three Dimensional
  • Turbines

Fields of Study

  • Physics

Readers

  • Internal Combustion Engine (ICE) Technology.
  • Theoretical Analysis.