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.
Aircraft Rocket Subsystems
1972
25 pages
Report
No indication
English
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