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.
Validation of OVERFLOW for Supersonic Retropropulsion
11th Symposium on Overset Composite Grids and Solution Technology ; 2012 ; Dayton, OH, United States
2012-10-15
Miscellaneous
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English
Validation of OVERFLOW for Supersonic Retropropulsion
NTIS | 2012
|Toward Supersonic Retropropulsion CFD Validation
AIAA | 2011
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