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VIKING DYNAMICS EXPERIENCE
APPLICATION TO FUTURE PAYLOADS
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acceleration accelerometers acoustic environment aeroshell analytical applied assembly attenuation axis base cover bioshield bolted joint calculated Centaur components configuration criteria Curve damping engine equipment plate evaluate fixture flight data flight measurements frequency range future payloads Hz Figure input interface joint Lander body landing shock LDTM LDTM/ODTM loads analysis margin max q maximum mission modal mode shapes modes mounted noise ODTM Orbiter Orbiter dynamic overall PC board peak PFLA predicted pressure primary structure propulsion pyro shock pyrotechnic pyrotechnic shock qualification test random vibration reduced response shaker shock environments shock spectra shock tests simulation sound pressure level strain gages structural loads subsystem system-level test techniques terminal descent test article test data test levels test program test spectrum tion Titan III transient truss verify vibration environment vibration test Viking Lander Viking Project Viking spacecraft