DEVELOPMENT OF NONDESTRUCTIVE TESTING TECHNIQUES FOR LARGE SOLID-PROPELLANT ROCKET MOTORS

Abstract

Contents: Relationship of chamber pressure to excess burning area Stress analysis of the propellant grain Defect analysis Determination of the pressure distribution in a propellant grain crack Temperature increase of the metal case resulting from premature exposure of the case insulation Method for determining the burning propellant surface area as a function of time based on an experimental combustion chamber pressure

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1962
Accession Number
AD0282439

Entities

People

  • David Baker
  • R. Citerley
  • S. A. Murch

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Burning Rate
  • Combustion
  • Combustion Chambers
  • Computational Fluid Dynamics
  • Computational Science
  • Difference Equations
  • Differential Equations
  • Elastic Properties
  • Heat Transfer
  • Materials
  • Mechanical Properties
  • Mechanics
  • Modulus Of Elasticity
  • Pressure Distribution
  • Stress Strain Relations
  • Stresses

Fields of Study

  • Physics

Readers

  • Rocket Propulsion.

Technology Areas

  • Microelectronics
  • Microelectronics - Graphene