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  1. 1
    Thermal structures technology development for reusable launch vehicle cryogenic propellant tanks /
    Published 1998
    Government Document Book
  2. 2
    Prediction of the ullage gas thermal stratification in a NASP vehicle propellant tank experimental simulation using FLOW-3D.
    by Hardy, Terry L.
    Published 1990
    Government Document Microform Book
  3. 3
    Flight control augmentation for AFT CG launch vehicles.
    by Barret, Chris
    Published 1996
    Government Document Book
  4. 4
    Reusable Launch Vehicle Technology Program /
    by Freeman, Delma C.
    Published 1996
    Government Document Book
  5. 5
    Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept /
    by Rivers, H. Kevin
    Published 1999
    Government Document Book
  6. 6
    Testing of densified liquid hydrogen stratification in a scale model propellant tank /
    by Jurns, John M.
    Published 2001
    Adobe Acrobat Reader required
    Government Document Book
  7. 7
    Analysis of tank PMD rewetting following thrust resettling /
    by Weislogel, Mark M.
    Published 2002
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    Government Document Microform Book
  8. 8
    Tank pressure control experiment on the space shuttle.
    Published 1989
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    Government Document Book
  9. 9
    Independent Orbiter assessment : assessment of the electrical power generation/power reactant storage and distribution subsystem FMEA/CIL /
    by Ames, B. E.
    Published 1988
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    Government Document Book
  10. 10
    Ion thruster system (8-CM) cyclic endurance test /
    Published 1984
    Government Document Microform Book
  11. 11
    Computational Fluid Dynamics (CFD) simulations of jet mixing in tanks of different scales /
    by Breisacher, Kevin J.
    Published 2010
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    Government Document Conference Proceeding eBook
  12. 12
    Liquid oxygen propellant densification production and performance test results with a large-scale flight-weight propellant tank for the X33 RLV /
    by Tomsik, Thomas M.
    Published 2010
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    Government Document eBook
  13. 13
    Cryogenic propellant management device conceptual design study /
    Published 2010
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    Government Document eBook
  14. 14
    A densified liquid methane delivery system for the Altair ascent stage /
    Published 2010
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    Government Document Conference Proceeding eBook
  15. 15
    Hypervelocity impact of unstressed and stressed titanium in a Whipple configuration in support of the Orion Crew Exploration Vehicle Service Module propellant tanks /
    Published 2010
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    Government Document Conference Proceeding eBook
  16. 16
    Thermal structures technology development for reusable launch vehicle cryogenic propellant tanks /
    Published 2005
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    Government Document eBook
  17. 17
    Evaluation of aluminum alloy 2050-T84 microstructure and mechanical properties at ambient and cryogenic temperatures /
    Published 2011
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    Government Document eBook
  18. 18
    Model of the radio frequency (RF) excitation response from monopole and dipole antennas in a large scale tank /
    by Wilson, Jeffrey D.
    Published 2012
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    Government Document eBook
  19. 19
    Issues of long-term cryogenic propellant storage in microgravity /
    by Muratov, C. B.
    Published 2011
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    Government Document eBook
  20. 20
    Large-scale liquid hydrogen tank rapid chill and fill testing for the advanced shuttle upper stage concept /
    by Flachbart, R. H.
    Published 2013
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    Get full text
    Government Document eBook
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