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Inviscid flow computations of several aeroshell configurations for a '07 Mars lander [microform] / Ramadas K. Prabhu ; prepared for ... under contract NAS1-96014.
Text
Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
2001
0 resources
Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24 [microform] / Ramadas K. Prabhu ; [prepared ... under contract NAS1-00135].
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Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
2001
0 resources
Superalloy foams for aeroshell applications [microform] / John Gayda and Santo Padula II.
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Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information, [2001]
2001
1 resource
Available online
Adobe Acrobat Reader requiredAn inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5 [microform] / Ramadas K. Prabhu.
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Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information, [2001]
2001
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS39078Experimental study of convective heating on the back face and payload of a Hypersonic Inflatable Aerodynamic Decelerator (HIAD) aeroshell / Brian R. Hollis [and three others].
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Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2017.
2017-3
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo79528Finite element modeling and analysis of Mars entry aeroshell concept / Samee W. Ahmed, Brittney M. Lane.
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Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 2017.
2017-6
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo82527Mars Sample Return : Mars ascent vehicle mission & technology requirements / Jerrey V. Bowles, Loc C. Huynh, Veronica M. Hawke.
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Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, 2013.
2013
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo37989Entry, descent, and landing with propulsive deceleration : supersonic retropropulsion wind tunnel testing and shock phenomena / Bryan Palaszewski.
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Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2014.
2014-9
1 resource
Available online
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