U.S. Department of Defense MIL-STD-810D — vdj6225.tmp (EN)

Downloaded from https://www.everyspec.com MIL-STD-81OD ;. 19 July 1983 1-4.1 X.2stin erruD =. t t. If there is an unscheduled test interruption, the chamber shall be returned to ground level and purged to remove the flammable atmoshpere. The test shall be reinitiated from the point of interruption using the same test item. I-4.2 ~& Any interruption in the’test that results in a more extreme exposure ,ofthe teat item than required by the equipment specification should be followed by a complete physical inspection of the test -itemand an operational check prior to continuation of test.

An engineering judgment ehall be mqde whether to continue testing with the specific item given the overtest, to obtain a new item, or to consider the teat completed. I-4.3 ~lure ~. All failures (see I-4.4) and incidents where the test items do not meet the equipment operating requirements shall be ana~yzed to determine the cause and impact-of such occurrences. Correctiveactions shall be proposed or implemented as required to meet equipment performance requirements. I-4.4 l?ailurecr&2c&. a. Procedure”I - Ignitioriof test “fuelvapor and air environment’ constitutesfailure of the test. b.

Procedure II - Propagation of flame to, or ignition or, a flanuoabie atmosphere surrounding the test item when the test atmosphere tiithinthe enclosure or case of the test item is intentionally ignited constitutes failure / of the test. ,. I-4.5 .SummervOf Inform io~. t The following information“isrequired in the test plan for the conduct of the tests of Section II: Test altitudes b. Test temperatures c. Fuel volume snd/oi weight d. Test item configuration EEmE@s I-5 Haskin, W.L. Proof Test~. 1963. ASD-T%-62-1OE1 ~ DTIC number AD-400-483. b. Zabetakis, M.G.,.A.~. Furno, and G,W. Jones. **Minimum Spontaneous Ignition Temperatures of Combustibles in Air,w ,. ~ 46 (1954),2173-2178. . c.

Washburn, E.W., ed. es of N~ ~. VO1. III, New York: National Research Council/ McGraw-Hill, 1928. Pp 27-29~ d. Kuchta, J .M. Summarv~ltlon Properties of Jet Fuels and Oh Aircraft Cx@ustible Flu. 1975. AFAPL-TR-75-70, PP 9-14. DTIC number AD-Ao21-320. e. ASTM E 380-79. rd for Metric Practice. MSTHOD 5il.2 511.2-5 19 July 1983