Showing 1 - 19 results of 19 for search '', query time: 0.09s Refine Results
  1. 1
    Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure

    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


    Save to List
    Saved in:
  2. 2
    High altitude chemically reacting gas particle mixtures. Volume III, Computer code user's and applications manual

    High altitude chemically reacting gas particle mixtures. Volume III, Computer code user's and applications manual by Smith, S. D. (Sheldon D.)

    Huntsville, AL : Lockheed Missiles & Space Company, Huntsville Research & Engineering Center, 1984
    Format: Government Document Book


    Save to List
    Saved in:
  3. 3
    Multidisciplinary approach to aerospike nozzle design

    Multidisciplinary approach to aerospike nozzle design

    Hampton, Va. : [Springfield, Va.] :; Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


    Save to List
    Saved in:
  4. 4
    Performance of an axisymmetric rocket based combined cycle engine during rocket only operation using linear regression analysis

    Performance of an axisymmetric rocket based combined cycle engine during rocket only operation using linear regression analysis

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


    Save to List
    Saved in:
  5. 5
    Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure

    Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure by Jankovsky, Robert S.

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


    Save to List
    Saved in:
  6. 6
    High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation

    High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation by Jankovsky, Robert S.

    [Cleveland, Ohio] : [Springfield, Va.] : National Aeronautics and Space Administration, Glenn Research Center ; [National Technical Information Service, distributor], 1999
    Format: Government Document Book


    Save to List
    Saved in:
  7. 7
    Shelf life extension for the lot AAE nozzle severance LSCs : final test report

    Shelf life extension for the lot AAE nozzle severance LSCs : final test report by Cook, M.

    Brigham City, UT : [Marshall Space Flight Center, Ala..] :; Brigham City, UT : [Marshall Space Flight Center, Ala. :] : Thiokol Corp., Space Operations ; [National Aeronautics and Space Administration, George C. Marshall Space Flight Center?], 1990
    Format: Government Document Book


    Save to List
    Saved in:
  8. 8
    Development of thermal barriers for solid rocket motor nozzle joints

    Development of thermal barriers for solid rocket motor nozzle joints by Steinetz, Bruce M.

    [Cleveland, Ohio] : [Springfield, Va.] : National Aeronautics and Space Administration, Glenn Research Center ; [National Technical Information Service, distributor], 1999
    Format: Government Document Book


    Save to List
    Saved in:
  9. 9
    Star 48 solid rocket motor nozzle analyses and instrumented firings

    Star 48 solid rocket motor nozzle analyses and instrumented firings by Porter, Robert L.

    [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


    Save to List
    Saved in:
  10. 10
    A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center

    A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center by Davidian, Kenneth J.

    [Washington, D.C.?] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1987
    Format: Government Document Book


    Save to List
    Saved in:
  11. 11
    Final report for the NASA reload program

    Final report for the NASA reload program

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


    Save to List
    Saved in:
  12. 12
    Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle.

    Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle. by Marable, R. W.

    [West Palm Beach, Fla.] : [Washington, DC] : [Springfield, Va.] : [Pratt and Whitney Aircraft] ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1989
    Format: Government Document Book


    Save to List
    Saved in:
  13. 13
    Advanced small rocket chambers option 3 : 110 1bf Ir-Re rocket

    Advanced small rocket chambers option 3 : 110 1bf Ir-Re rocket by Jassowski, Donald M.

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


    Save to List
    Saved in:
  14. 14
    High performance solid rocket motor (SRM) submerged nozzle-combustion cavity flowfield assessment : final report

    High performance solid rocket motor (SRM) submerged nozzle-combustion cavity flowfield assessment : final report

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


    Save to List
    Saved in:
  15. 15
    Final postflight hardware evaluation report, 360T021 (RSRM-21, STS-45).

    Final postflight hardware evaluation report, 360T021 (RSRM-21, STS-45).

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


    Save to List
    Saved in:
  16. 16
    A performance comparison of two small rocket nozzles

    A performance comparison of two small rocket nozzles by Arrington, Lynn A.

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


    Save to List
    Saved in:
  17. 17
    Flight motor set 360L002 (STS-27R). Volume 5. Nozzle component : final report

    Flight motor set 360L002 (STS-27R). Volume 5. Nozzle component : final report by Meyer, S. A.

    Brigham City, UT : Marshall Space Flight Center, Ala. :; Brigham City, UT : Marshall Space Flight Center, Ala. : Thiokol Corp., Space Operations ; National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1989
    Format: Government Document Book


    Save to List
    Saved in:
  18. 18
    Comparison of response surface and kriging models in the multidisciplinary design of an aerospike nozzle

    Comparison of response surface and kriging models in the multidisciplinary design of an aerospike nozzle by Simpson, Timothy W.

    Hampton, Va. : Springfield, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; National Technical Information Service, distributor, 1998
    Format: Government Document Book


    Save to List
    Saved in:
  19. 19
    Large-displacement structural durability analyses of simple bend specimen emulating rocket nozzle liners

    Large-displacement structural durability analyses of simple bend specimen emulating rocket nozzle liners by Arya, Vinod K.

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


    Save to List
    Saved in:

Search Tools: