JOTP-011
5 December 2014
APPENDIX A. BACKGROUND/RATIONALE
ANNEX 1. ENVIRONMENTAL TESTS
A.1-3.6.1 Launch Shock (Appendix C, Annex 2, Paragraph C.2-10.1).
Launch shock should be conducted in accordance with MIL-STD-810, Methods 516 and 525 as
appropriate; however, tailored test levels based on measured data will normally be used. Test
severities should be derived in accordance with MIL-STD-810, Method 514, Annex F.
A.1-3.6.2 Free Flight Vibration (Appendix C, Annex 2, Paragraph C.2-10.2).
Free flight vibration testing should be conducted in accordance with MIL-STD-810, Methods 514
and 525 as appropriate; however, tailored test levels based on measured data will normally be used.
Test severities should be derived in accordance with MIL-STD-810, Method 514, Annex F.
A.1-21
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