Research Catalog

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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

  • 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].

    • Text
    • Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001

  • Superalloy foams for aeroshell applications [microform] / John Gayda and Santo Padula II.

    • Text
    • 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

    http://purl.access.gpo.gov/GPO/LPS30325

  • An 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.

    • Text
    • 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/LPS39078

  • Experimental study of convective heating on the back face and payload of a Hypersonic Inflatable Aerodynamic Decelerator (HIAD) aeroshell / Brian R. Hollis [and three others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2017.
    • 2017-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo79528

  • Finite element modeling and analysis of Mars entry aeroshell concept / Samee W. Ahmed, Brittney M. Lane.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 2017.
    • 2017-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo82527

  • Mars Sample Return : Mars ascent vehicle mission & technology requirements / Jerrey V. Bowles, Loc C. Huynh, Veronica M. Hawke.

    • Text
    • Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, 2013.
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37989

  • Entry, descent, and landing with propulsive deceleration : supersonic retropropulsion wind tunnel testing and shock phenomena / Bryan Palaszewski.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2014.
    • 2014-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo56718

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