Research Catalog

  • Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept [microform] / H. Kevin Rivers.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999
  • Trade study plan for reusable hydrogen composite tank system (RHCTS) [microform] / H.S. Greenberg, principal investigator.

    • Text
    • [Downey, Calif.] : Rockwell Aerospace, Space Systems Division ; [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Milestone 4 [microform] : test plan for reusable hydrogen composite tank system (RHCTS) : task 3, composite tank materials / H.S. Greenberg, principal investigator.

    • Text
    • [Downey, Calif.] : Rockwell Aerospace, Space Systems Division ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Final technical report for multi-dimensional modeling of pressurization and expulsion of multi-phase hydrogen propellant [microform] : NASA grant NAG3-1292 / principal investigator, John I. Hochstein.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993
  • Prediction of the ullage gas thermal stratification in a NASP vehicle propellant tank experimental simulation using FLOW-3D [microform] / Terry L. Hardy and Thomas M. Tomsik.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
  • Flight control augmentation for AFT CG launch vehicles [microform] / Chris Barret.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Reusable Launch Vehicle Technology Program [microform] / Delma C. Freeman, Jr.; Theodore A. Talay; R. Eugene Austin.

    • Text
    • Paris, France : American International Astronautical Federation ; [Washington, D.C.] : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Thermal structures technology development for reusable launch vehicle cryogenic propellant tanks [microform] / by Theodore F. Johnson ... [et al.].

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Final report for the liquid motion in a rotating tank experiment (LME) [microform] / D.M. Deffenbaugh, F.T. Dodge, and S.T. Green.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Testing of densified liquid hydrogen stratification in a scale model propellant tank [microform] / John M. Jurns, Thomas M. Tomsik, William D. Greene.

    • 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/LPS30323
  • Analysis of tank PMD rewetting following thrust resettling [microform] / M.M. Weislogel, M.A. Sala, [and] S.H. Collicott.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS51555
  • Independent Orbiter assessment [microform] : assessment of the electrical power generation/power reactant storage and distribution subsystem FMEA/CIL / [prepared by B.E. Ames].

    • Text
    • Houston, Tex. : McDonnell Douglas Astronautics Company, Houston Division ; [Washington, DC : National Aeronautics and Space Administration, 1988]
    • 1988
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS70326
  • Tank pressure control experiment on the space shuttle [microform].

    • Text
    • [Cleveland, Ohio : NASA Lewis Research Center, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS70393
  • Ion thruster system (8-CM) cyclic endurance test [microform] / C.R. Dulgeroff, ... [et al.].

    • Text
    • Malibu, CA : Hughes Research Laboratories ; Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1984]
    • 1984
  • Model of the radio frequency (RF) excitation response from monopole and dipole antennas in a large scale tank / Jeffrey D. Wilson and Gregory A. Zimmerli.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo25030
  • Issues of long-term cryogenic propellant storage in microgravity / C.B. Muratov, V.V. Osipov, V.N. Smelyanskiy.

    • Text
    • Moffett Field, CA : National Aeronautics and Space Administration, NASA Ames Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo30651
  • Pressure-volume-temperature (PVT) gauging of an isothermal cryogenic propellant tank pressurized with gaseous helium / Neil T. Van Dresar and Gregory A. Zimmerli.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2014.
    • 2014-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo57361
  • Tank system integrated model : a cryogenic tank performance prediction program / L.G. Bolshinskiy [and five others].

    • Text
    • Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, April 2017.
    • 2017-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo82366
  • Testing of densified liquid hydrogen stratification in a scale model propellant tank / John M. Jurns, Thomas M. Tomsik, William D. Greene.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2001.
    • 2001-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS30323
  • Large-scale liquid hydrogen tank rapid chill and fill testing for the advanced shuttle upper stage concept / R.H. Flachbart [and six others].

    • Text
    • Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, 2013.
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37982

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