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  1. 1
    Prediction of pressurant mass requirements for axisymmetric liquid hydrogen tanks

    Prediction of pressurant mass requirements for axisymmetric liquid hydrogen tanks by Van Dresar, N. T.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  2. 2
    Oxygen consumption of tilapia and preliminary mass flows through a prototype closed aquaculture system

    Oxygen consumption of tilapia and preliminary mass flows through a prototype closed aquaculture system by Muller, M. S.

    Kennedy Space Center, Fla. : [Springfield, Va.] : National Aeronautics and Space Administration, John F. Kennedy Space Center ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


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  3. 3
    Performance of the active sidewall boundary-layer removal system for the Langley 0.3-meter transonic cryogenic tunnel

    Performance of the active sidewall boundary-layer removal system for the Langley 0.3-meter transonic cryogenic tunnel by Balakrishna, S., 1931-

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1989
    Format: Government Document Book


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  4. 4
    Mass loss in the interacting semi-detached binary delta librae

    Mass loss in the interacting semi-detached binary delta librae by McCluskey, G. E. (George E.)

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  5. 5
    Towards a theory of tropical/midlatitude mass exchange from the Earth's surface through the stratosphere : progress report for year one, 12/1/94-9/30/95

    Towards a theory of tropical/midlatitude mass exchange from the Earth's surface through the stratosphere : progress report for year one, 12/1/94-9/30/95 by Hartley, Dana

    [Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  6. 6
    Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction

    Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction by Davis, D. O.

    [Cleveland, Ohio] : Springfield, VA : National Aeronautics and Space Administration, Lewis Research Center ; National Technical Information Service, distributor, 1998
    Format: Government Document Book


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  7. 7
    Leading edge film cooling effects on turbine blade heat transfer

    Leading edge film cooling effects on turbine blade heat transfer by Garg, Vijay Kumar, 1938-

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  8. 8
    Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber

    Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber by Wadel, Mary F.

    [Washington, DC] : [Springfield, Va.] :; [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


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  9. 9
    Redesigned gas mass flow sensors for space shuttle pressure control system and fuel cell system : NASA contract no. NAS9-19322.

    Redesigned gas mass flow sensors for space shuttle pressure control system and fuel cell system : NASA contract no. NAS9-19322.

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


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  10. 10
    A full Navier-Stokes analysis of subsonic diffuser of a bifurcated 70/30 supersonic inlet for high speed civil transport application

    A full Navier-Stokes analysis of subsonic diffuser of a bifurcated 70/30 supersonic inlet for high speed civil transport application by Kapoor, Kamlesh

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


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  11. 11
    Ejector noise suppression with auxiliary jet injection : under contract NAS3-27246

    Ejector noise suppression with auxiliary jet injection : under contract NAS3-27246 by Berman, Charles H.

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


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  12. 12
    Mixing enhancement by tabs in round supersonic jets

    Mixing enhancement by tabs in round supersonic jets by Seiner, John M.

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1998
    Format: Government Document Book


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  13. 13
    Mass flow meter using the triboelectric effect for measurement in cryogenics : NASA contract NAS324648 : final report, April, 1987

    Mass flow meter using the triboelectric effect for measurement in cryogenics : NASA contract NAS324648 : final report, April, 1987 by Bernatowicz, H.

    Sunnyvale, CA : [Washington, DC] : [Springfield, Va.] : Science Applications International Corporation ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1987
    Format: Government Document Book


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  14. 14
    Mass flow measurement of liquid cryogens using the triboelectric effect : NASA contract NA83-24873, final report, August 12, 1986

    Mass flow measurement of liquid cryogens using the triboelectric effect : NASA contract NA83-24873, final report, August 12, 1986 by Dechene, Ronald L.

    Danvers, Mass. : [Washington, DC] : [Springfield, Va.] : Auburn International, Inc. ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1986
    Format: Government Document Book


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  15. 15
    Mixing of multiple jets with a confined subsonic crossflow. Part II, opposed rows of orifices in rectangular ducts

    Mixing of multiple jets with a confined subsonic crossflow. Part II, opposed rows of orifices in rectangular ducts by Holdeman, J. D.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


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