Contents: Vibroacoustic environmental simulation for aerospace vehicles; RTD sonic fatigue facility, design and performance characteristics; Operational characteristics of a 100,000-cubic-foot acoustic reverberation chamber; Concept, design, and performance of the spacecraft acoustic laboratory; Theoretical study of acoustic simulation of in-flight environments; Data handling methods for large vehicle testing; Development and verification of the vibration test requirements for the Apollo command and service modules; Development and verification of the Apollo lunar module vibration test requirements; Saturn S-II, S-IVB, and instrument unit subassembly and assembly vibration and acoustic evaluation programs; Development of acoustic test conditions for Apollo lunar module flight certification; Facility sonic fatigue proof testing; Vibroacoustic test methods for vibration qualification of Apollo flight hardware; Acoustical qualification of S-IC fin structures; Simulation of acoustic fatigue failure in the wideband noise test facility of the Air Force Flight Dynamics Laboratory; Real-time combined acoustic-vacuum testing of spacecraft.
The Shock and Vibration Bulletin
1968
184 pages
Report
No indication
English
Structural Mechanics , Information Systems , Aircraft , Manned Spacecraft , Shock(Mechanics) , Vibration , Symposia , Impact shock , Fluid dynamic properties , Spacecraft , Cratering , Physical properties , Transducers , Nuclear explosion damage , Stresses , Elasticity , Attenuation , X-ray absorption analysis , Acoustic properties , Shear stresses , Viscosity , Acceleration , Mathematical analysis , Simulation , Helicopters
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