Simulated Air Launch Environment, Volume 2. Aeroheat Data Summary

Abstract

A program was conducted in which the response and failure charactersitcs of solid propellant rocket motors when subjected to transient thermal conditions representing air launch operational environments were recorded and analyzed. Future Air Force mission profiles were used. The Maverick motor, AGM-65A, was used as a test bed on the program.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1974
Accession Number
ADB010173

Entities

People

  • O. R. Pritts

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Contracts
  • Environment
  • Government Procurement
  • Governments
  • Mission Profiles
  • Missions
  • Physical Properties
  • Procurement
  • Rocket Engines
  • Shear Stresses
  • Solid Propellants
  • Stress Analysis
  • Stresses
  • Test And Evaluation
  • Test Beds

Readers

  • Aerospace logistics and air mobility.
  • Rocket Propulsion.