Research Catalog

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  • Parametric entry corridors for lunar/mars aerocapture missions / Lisa Ling, Franco M. Baseggio, Douglas P. Fuhry.

    • Text
    • Houston, Tex. : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 1991.
    • 1991

  • Nonequilibrium radiation and chemistry models for aerocapture vehicle flowfields [microform] : semiannual progress report, February 1991 - June 1991 / Leland A. Carlson.

    • Text
    • College Station, TX : Aerospace Engineering Dept., Texas A&M University ; [Washington, D.C. : National Aeronautics and Space Administration, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS59936

  • Nonequilibrium radiation and chemistry models for aerocapture vehicle flowfields [microform] : semiannual progress report, January 1990--June 1990 / Leland A. Carlson.

    • Text
    • College Station, TX : Aerospace Engineering Dept., Texas A&M University ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS64094

  • Analytical guidance law development for aerocapture at Mars [microform] : progress report #4 / principal investigator: A.J. Calise.

    • Text
    • Atlanta, Ga. : School of Aerospace Engineering, Georgia Institute of Technology ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69363

  • Advanced orbit transfer vehicle propulsion system study [microform] : final report / J.A. Cathcart ... [et al.].

    • Text
    • Denver, Colo. : Martin Marietta Aerospace, [1985]
    • 1985

  • Mars global reference atmospheric model 2010 version users guide / H.L. Justh.

    • Text
    • Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, February 2014.
    • 2014-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo54353

  • Modeling of aerobrake ballute stagnation point temperature and heat transfer to inflation gas / Parviz A. Bahrami.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37271

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