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MIL-STD-2102A, DEPARTMENT OF DEFENSE TEST METHOD STANDARD: AIRCREW ESCAPE PROPULSION SYSTEMS; VIBRATION AND SHOCK TESTS FOR (18 AUG 1980)

MIL-STD-2102A, DEPARTMENT OF DEFENSE TEST METHOD STANDARD: AIRCREW ESCAPE PROPULSION SYSTEMS; VIBRATION AND SHOCK TESTS FOR (18 AUG 1980)., This standard establishes vibration and shock tests of aircrew escape propulsion systems (AEPS) to determine if the systems are constructed to withstand dynamic vibration and shock stresses expected during service use, handling, and transportation.

MIL-STD-2102 Rev. A

    

Version:
A08-199119.09 KB MIL-STD-2102A_NOTICE-2
A06-198627.93 KB MIL-STD-2102A_NOTICE-1
A08-1980516.66 KB MIL-STD-2102A

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