JOTP-011
5 December 2014
APPENDIX C. ENVIRONMENTAL TEST DESCRIPTIONS
ANNEX 2. DYNAMIC TESTS
a. Test Configuration: Attach the munition to the vibration exciter in all relevant tactical
launcher transport or deployment configurations.
b. Test Level: Vibration test each munition in accordance with the vibration test schedule
representative of the munition location on the platform. Vibration specification development
guidance is provided in MIL-STD-810, Method 514, Annex F.
c. Test Duration: The required test duration is dependent upon the munition life cycle but
should be equivalent to at least 1000 km of transport in this configuration.
d. Test Temperature: Temperature condition the test munitions prior to, and during
vibration testing. Stabilize all cold munitions to -46 °C, and all hot munitions to the SRE
temperature.
C.2-5.1.4 Tactical Launcher Shocks.
Perform shock testing in accordance with MIL-STD-810, Method 516 using the following test
parameters:
a. Test Configuration: Attach the munition to the shock exciter in all relevant tactical
launcher transport or deployment configurations.
b. Test Level: Shock test each munition to a tailored shock response spectrum (SRS)
representative of the launcher location on the platform(s). SRS specification development
guidance is provided in MIL-STD-810, Method 514, Annex F. This test may be eliminated if
determined to be sufficiently benign compared to other dynamic environments.
c.
Number of Shocks: The required number of shocks is determined by the LCEP.
d. Test Temperature: Temperature condition the test munitions prior to, and during shock
testing. Stabilize all cold munitions to -46 °C, and all hot munitions to the SRE temperature.
C.2-5.1.6 Adjacent Munition Firing Shocks.
Perform shock testing in accordance with MIL-STD-810, Method 514 using the following test
parameters:
a. Test Configuration:
Attach the munition to the shock exciter in the launch
configuration.
b. Test Level: Shock test each munition to a tailored shock response spectrum (SRS)
representative of the launcher location on the platform(s). SRS specification development
guidance is provided in MIL-STD-810, Method 514, Annex F. This test may be eliminated if
C.2-11
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