Aircraft Rocket Subsystems

Abstract

The report describes a method for the evaluation of air to ground rocket subsystem performance characteristics. It provides procedures for test preparation, physical characteristics, safety evaluation, high temperature (+145 deg F), low temperature (-50 deg F), sand, dust, humidity, salt spray, fungus, rain, freezing rain, vibration, static loading, firing tests, durability, accuracy, and dispersion.

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Document Details

Document Type
Technical Report
Publication Date
Jan 15, 1972
Accession Number
AD0737177

Entities

Organizations

  • United States Army Test and Evaluation Command

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Aircrafts
  • Airframes
  • Bomb Racks
  • Cameras
  • Climate Change
  • Engineering
  • Environmental Tests
  • Measurement
  • Photographic Equipment
  • Photographs
  • Photography
  • Rocket Engines
  • Rocket Launchers
  • Rotary Wing Aircraft
  • Test And Evaluation
  • Test Methods

Fields of Study

  • Engineering

Readers

  • Aerosol Science/Aerosol Physics
  • Aerospace Test and Evaluation
  • Thermal Physics or Thermal Science.