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    Validation of OVERFLOW for Supersonic Retropropulsion (2012)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: The goal is to softly land high mass vehicles (10s of metric tons) on Mars. Supersonic Retropropulsion (SRP) is a potential method of deceleration. Current method of supersonic parachutes does not scale past ~1 metric ton. CFD is of increasing importance since flight and experimental data at these conditions is difficult to obtain. CFD must first be validated at these conditions.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: JSC-CN-27217 , 11th Symposium on Overset Composite Grids and Solution Technology; Oct 15, 2012 - Oct 18, 2012; Dayton, OH; United States
    Format: application/pdf
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