A summary of spacecraft loads data from four Titan Centaur launch vehicle flights

Computer Science

Scientific paper

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Dynamic Loads, Helios A, Titan Launch Vehicles, Viking Lander Spacecraft, Acoustics, Environmental Tests, Shock Waves, Tables (Data), Vibration

Scientific paper

The payloads carried by the first four Titan Centaur Launch Vehicle flights were a Viking Spacecraft Dynamic Simulator, the Helios-A Spacecraft and the the two Viking Spacecraft. Dynamic loads data were gathered by the NASA Viking Project Office from these four flights. These data are summarized and compared with Viking design requirements. Recommendations on design and test requirements for general spacecraft application are presented.

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