A Computer Program for Prediction of Internal Performance of a Ramrocket

Abstract

The operation of a computer program to predict idealised ramrocket performance is described. The program predicts performance for chosen aerodynamic and thermodynamic variables and contains provision for varying the gas generator propellant formulation.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1991
Accession Number
ADA238179

Entities

People

  • Lincoln P. Erm

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Chambers
  • Chemical Properties
  • Combustion
  • Combustion Chambers
  • Combustion Products
  • Computer Programs
  • Computers
  • Flow
  • Generators
  • Heat Of Formation
  • Mach Number
  • Mass Flow
  • Secondary Flow
  • Specific Heat
  • Specific Impulse
  • Static Pressure

Fields of Study

  • Physics

Readers

  • Computational Modeling and Simulation
  • Rocket Propulsion.