Research Catalog

  • Experimental and analytical comparison of flowfields in a 110 N (25 Lbf) H₂/O₂ rocket [microform] / Brian D. Reed ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, [1991]
    • 1991
  • A performance comparison of two small rocket nozzles [microform] / Lynn A. Arrington, Brian D. Reed, Angel Rivera, Jr.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Preliminary results of solid gas generator micropropulsion [microform] / Wilhelmus A. de Groot, Brian D. Reed, Marshall Brenizer.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999
  • Perormance comparison of axisymmetric and three-dimensional hydrogen film coolant injection in a 110N hydorgen-oxygen rocket [microform] / Lynn A. Arrington and Brian D. Reed.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1992?]
    • 1992
  • A performance comparison of two small rocket nozzles / Lynn A. Arrington, Brian D. Reed, Angel Rivera, Jr.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, August 1996.
    • 1996-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo67112

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