Contents: Estimate of effect of spacecraft vibration qualification testing on reliability; S-IC reliability program from structural life viewpoint; Structural reliability - panel session; Dynamic analysis of ATS-B spacecraft; Spacecraft design for atlas torsional shock transient; Comparison of predicted and measured launch loads for snap 10A; Ground-wind-induced oscillations of Gemini-Titan air vehicle and its erector; Noise level measurements for improved delta, Atlas/Agena-D, and TAT/Agena-D launch vehicles; The 'Vacuum spring'; Self-adaptive vibration balancing device for helicopters; Shock response of electronic equipment cabinets by normal mode method; Damped vibrations of elastically supported rigid body with coupling between translation and rotation; Missile handling analysis.
The Shock and Vibration Bulletin
1967
154 pages
Report
Keine Angabe
Englisch
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