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MIL-STD-2102A (NOTICE 1), DEPARTMENT OF DEFENSE TEST METHOD STANDARD: AIRCREW ESCAPE PROPULSION SYSTEMS; VIBRATION AND SHOCK TESTS FOR (20 JUN 1986)

MIL-STD-2102A (NOTICE 1), DEPARTMENT OF DEFENSE TEST METHOD STANDARD: AIRCREW ESCAPE PROPULSION SYSTEMS; VIBRATION AND SHOCK TESTS FOR (20 JUN 1986)., MIL-STD-2102A(NAVY), dated 18 August 1980, has been reviewed and determined to be valid for use in acquisition.

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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