JOTP-011
5 December 2014
APPENDIX C. ENVIRONMENTAL TEST DESCRIPTIONS
ANNEX 2. DYNAMIC TESTS
Subject three (3) test munitions to the Logistic Drop Test with a criterion of Safe for Disposal.
Perform drop testing in accordance with MIL-STD-2105 using the following test parameters:
a. Munition Configuration: The munitions are tested in the packaged configuration unless
the potential exists for munitions to be handled out of the shipping container while on naval
vessels. In this case the munitions are required to be tested in the unpackaged mode.
b.
Test Level: One drop of 12 m onto a concrete supported steel surface.
c. Drop Orientations: Each test munition to impact in one of the following orientations.
(Note sample size should be sufficient to ensure that all orientations are addressed):
(1) Major axis horizontal
(2) Major axis vertical, nose up / base down
(3) Major axis vertical, nose down / base up
d.
Test Temperature: Ambient
C.2-10 MUNITION FLIGHT DYNAMICS.
Munition Flight Dynamics addresses the mechanical environments that may be encountered during
missile and rocket launch and flight. Test levels are to be tailored from measured data.
C.2-10.1 Launch Shock.
Launch shock should be conducted in accordance with MIL-STD-810, Methods 516 and 525
appropriate; however, tailored test levels based on measured data will normally be used. Replicate
all shocks occurring within the safe separation zone. This may include shocks caused by safe entry
into water or multi stage rocket motor separation / ignition events. Derive test severities in
accordance with MIL-STD-810, Method 514, Annex F.
a.
Test Configuration. Attach the munition to the shock exciter as appropriate.
b. Test Level. The tailored test levels are typically specified as either a half-sine shock
pulse or a shock response spectra in accordance with Method 516 (SRS).
C.2-15
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