Research Catalog

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  • Risk analysis of earth return options for the Mars Rover/sample return mission [microform].

    • Text
    • Webster, Tex. : Eagle Engineering, Inc. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • Self-adaptive difference method for the effective solution of computationally complex problems of boundary layer theory [microform] / W. Schönauer ... [et al.].

    • Text
    • Washington, DC : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Rarefied gas effects on aerobraking/reentry vehicles with wakes [microform] / prepared by Amolak C. Jain.

    • Text
    • [Huntsville, AL] : Remtech ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • A vehicle health monitoring system for the space shuttle reaction control system during reentry [microform] / by Anthony David Rosello.

    • Text
    • Cambridge, Mass. : Charles Stark Draper Laboratory ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Orbiter rarefied-flow reentry measurements from the OARE on STS-62 [microform] / R.C. Blanchard, J.Y. Nicholson.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Convective and radiative heating for vehicle return from the Moon and Mars [microform] / R.B. Greendyke, P.A. Gnoffo.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Development of the reentry flight dynamics simulator for evaluation of Space Shuttle Orbiter entry systems / Lawrence F. Rowell, Richard W. Powell, and Howard W. Stone, Jr.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, October 1980.
    • 1980-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70979

  • 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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