Laboratory test is devised to approximate payload vibration response characteristics of Nike Tomahawk system; test is based upon flight test data and apparent weight (WA) characteristics of rocket motors and payload; intermediate tests gave data on payload's vibration response to motor burning irregularities; test procedure included also static firing, force controlled vibration testing and electric simulation of WA during force controlled test; test results and practical limitations of test procedure are considered.
Progress report on force controlled vibration testing
U S Naval Research Laboratory -- Shock Vibration Bul
1966
14 pages
Aufsatz (Zeitschrift)
Englisch
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