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  1. 1

    Final report on all shuttle Centaur engine and nozzle support plug vibration testing

    West Palm Beach, Fla. : [Washington, DC : Springfield, Va. : United Technologies, Pratt & Whitney ; National Aeronautics and Space Administration ; National Technical Information Service, distributor, 1987
    Format: Government Document Book


  2. 2

    Effective streams for fighting fires by Kimball, Warren Young

    Boston, Mass. : National Fire Protection Association, 1961
    1st ed.
    Format: Book


  3. 3

    Separation of isotope mixture by nozzle process by Mikami, Hisashi

    Oak Ridge, Tenn. : U.S. Atomic Energy Commission, Division of Technical Information, 1962
    Format: Government Document Book


  4. 4

    TMI-2 instrument nozzle examinations at Argonne National Laboratory : February 1991-June 1993

    Washington, DC : Division of Systems Research, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission : Supt. of Docs., U.S. G.P.O. [distributor], 1994
    Format: Government Document Book


  5. 5

    Arcjet nozzle design impacts by Curran, Francis M.

    [Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1989
    Format: Government Document Book


  6. 6

    Removal of halogens, carbon dioxide, and aerosols from air in a spray tower by Liimatainen, R. C.

    Argonne, Ill. : Argonne National Laboratory, Chemical Engineering Division, 1955
    Format: Government Document Book


  7. 7

    Qualification test of the Ross double planetary mixer : final test report by Lueders, K. F.

    Brigham City, UT : [Washington, DC] : [Springfield, Va.] : Thiokol Corp., Space Operations ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1993
    Format: Government Document Book


  8. 8

    A computational model for the prediction of jet entrainment in the vicinity of nozzle boattails (The BOAT code) by Dash, Sanford M.

    [Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Service ; For sale by the National Technical Information Service, 1978
    Format: Government Document Book


  9. 9

    Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m²(350 psia) by Smith, Tamara A.

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1987
    Format: Government Document Book


  10. 10

    An equation for predicting a mean drop size in a high-speed spray. by Harmon, Darell Boyd, 1921-

    Berkeley : University of California Press, 1955
    Format: Book


  11. 11

    Plastic fire nozzle evaluation.

    San Dimas, Calif. : Forest Service, U.S. Dept. of Agriculture, Equipment Development Center, 1970
    Format: Government Document Book


  12. 12

    Perfect bell nozzle parametric and optimization curves by Tuttle, J. L.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983
    Format: Government Document Book


  13. 13

    Simulated flight acoustic investigation of treated ejector effectiveness on advanced mechanical suppressors for high velocity jet noise reduction by Brausch, J. F.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1986
    Format: Government Document Book


  14. 14

    Standardization of the carbon-phenolic materials and processes. Volume 1, Experimental studies (for period 1 September 1985 to 31 August 1988) : final report by Hall, William B.

    Mississippi State, Miss. : Mississippi State University, 1988
    Format: Government Document Book


  15. 15

    Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure by Hussaini, M. Moin

    Hampton, Va. : [Springfield, Va.] :; Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


  16. 16

    Design and analysis report for the flight weight 20-inch Columbium secondary nozzle for the RL10 engine by Castro, J. H.

    Cleveland, Ohio : [Springfield, Va. : NASA Lewis Research Center ; For sale by the National Technical Information Service, 1987
    Format: Government Document Book


  17. 17

    Investigation of installation effects on single-engine convergent-divergent nozzles by Burley, James R.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982
    Format: Government Document Book


  18. 18

    Data report of wind tunnel tests : D8-45 nozzle atomizing glycerin [sic] and water at air velocities 50 and 60 MPH by Yates, Wesley E.

    Davis, Calif. : Forest Pest Management, 1987
    Format: Book


  19. 19

    Aerodynamic performance of flared fan nozzles used as inlets by Dietrich, Donald A.

    Washington : Springfield, Va. : U.S. National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1976
    Format: Government Document Book


  20. 20

    Fuselage and nozzle pressure distributions on a 1/12-scale F-15 propulsion model at transonic speeds by Pendergraft, Odis C.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1979
    Format: Government Document Book