BAG: A code for predicting the performance of a gas bag impact attenuation system for the Pathfinder lander

Computer Science – Performance

Scientific paper

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Computer Programs, Computerized Simulation, Cushions, Deceleration, Gas Bags, Landing Gear, Mars (Planet), Mars Landing, Nasa Programs, Payloads, Performance Prediction, Prediction Analysis Techniques, Spacecraft Landing, Viking Lander Spacecraft, Attenuators, Pneumatics, Rigid Structures

Scientific paper

The National Aeronautics and Space Administration (NASA) is planning to launch a network of scientific probes to Mars beginning in late 1996. The precursor to this network will be PATHFINDER. Decelerating PATHFINDER from the high speed of its approach to Mars will require the use of several deceleration techniques working in series. The Jet Propulsion Laboratory (JPL) has proposed that gas bags be used to cushion the payload's ground impact on Mars. This report presents the computer code, BAG, which has been developed to calculate the pneumatic performance of gas bag impact attenuators and the one-dimensional rigid-body dynamic performance of a payload during ground impact.

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