The suggested design utilizes a spherically blunted 45 degree half-angle forebody with a low- density, ablative heatshield. ... Hermann, R. J. and Lineberger, W. C. aquot;Mars Sample Return: Issues and Recommendations, aquot; Task Group on Issues in Sample ... 5Meyerson, R. E. and Cerimele, C. J. aquot;Aeroassist Vehicle Requirements for a Mars Rover/Sample Return Mission, aquot; ... 12Cheatwood, F. M. Gnoffo, P. A. aquot;Usera#39;s Manual for the Langley Aerothermodynamic Upwind Relaxation Algorithmanbsp;...
Title | : | 7th AIAA/ASME Joint Thermophysics and Heat Transfer Conference |
Author | : | |
Publisher | : | - 1998 |
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