Sets of missiles were subjected to two 10-min vibration tests under combined temperature-altitude environment; temperature ranged from 180F to -30F, and altitude was 40,000 ft; missile was checked for acceptable operation before, during, and after environmental test; missiles which operated satisfactorily after laboratory tests were satisfactory in flight tests; missiles which showed early laboratory test failures and were subsequently corrected, were also satisfactory in flight test; there was good correlation between laboratory tests and flight tests, to indicate value for debugging tests.
Elimination of substandard parts by environmental testing
U S Naval Research Laboratory -- Shock Vibration Bul
1966
7 pages
Report
Englisch
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