TRANSIENT CHAMBER PRESSURE AND THRUST IN SOLID ROCKET MOTORS

Abstract

An analysis of solid rocket motors was made in order to find the chamber pressure and thrust during the transient periods of buildup and decay. The results are differential equations and solutions of closed form.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1965
Accession Number
AD0613962

Entities

People

  • Hans H. Seidel

Tags

DTIC Thesaurus Topics

  • Burning Rate
  • Chambers
  • Combustion
  • Combustion Chambers
  • Differential Equations
  • Engineering
  • Equations
  • Flow
  • Flow Rate
  • Ignition
  • Mass Flow
  • Nozzles
  • Rocket Engines
  • Solid Propellants
  • Specific Heat
  • Steady Flow
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Rocket Propulsion.