STUDY OF MECHANICAL PROPERTIES OF SOLID ROCKET PROPELLANTS. APPENDIXES A THROUGH G

Abstract

Contents: Analytical determination of generalized, linear viscoelastic stress-stain reations from uniaxial, biaxial, and triaxial experimental creep and relaxation data. Survey and development of methods for the de termination of strains in solid propellants. Parameter calculations of simple propellant grains for temperature cycling, pressuriza tion, and acceleration. Stress analysis of propellant grains using dis placement equations. Finite difference solution of ordinary and partial differential equations. Studies relating to structural analysis of solid propellants. Investigation of the failure of solid fuels under combined stresses.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1962
Accession Number
AD0281851

Entities

People

  • A. J. Durelli
  • Harry H. Hilton

Organizations

  • Aerojet Rocketdyne Holdings

Tags

Communities of Interest

  • C4I
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Composite Materials
  • Computational Science
  • Crystal Structure
  • Difference Equations
  • Differential Equations
  • Elastic Properties
  • Materials Laboratories
  • Materials Science
  • Materials Testing
  • Measurement
  • Mechanical Properties
  • Mechanics
  • Modulus Of Elasticity
  • Rocket Propellant Grains
  • Stress Strain Relations
  • Three Dimensional
  • Two Dimensional

Readers

  • Calculus or Mathematical Analysis
  • Mechanical Engineering/Mechanics of Materials.
  • Rocket Propulsion.