Research Catalog

New! Try our Article Search to discover online journals, books, and more from home with your library card.

Selected filters.Clear Filters

  • High pressure, earth-storable rocket technology [microform] / D.M. Jassowski.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration] ; Springfield, VA : National Technical Information Service [distributor, 1997-
    • 1997-present

  • Performance evaluation of a 50 kW Hall thruster [microform] / David T. Jacobson, Robert S. Jankovsky.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Two-dimensional converging-diverging rippled nozzles at transonic speeds [microform] / John R. Carlson and Scott C. Asbury.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • A first scramjet study [microform] / George Emmanuel.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Experimental and theoretical study of propeller spinner-shank interference [microform] / a thesis by Carl Clayton Cornwell.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Voyager 0.2-lbf thruster valve assembly [microform] : short pulse test report / prepared by Rocket Research Company ; prepared and approved by D.R. Johnson.

    • Text
    • Redmond, Wash. : The Company ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Investigation of wing upper surface flow-field disturbance due to NASA DC-8-72 in-flight inboard thrust-reverser deployment [microform] / Hedayat U. Hamid, Richard J. Margason, and Gordon Hardy.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • High-speed engine/component performance assessment using exergy and thrust-based methods [microform] / D.W. Riggins.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • An investigation of nonlinear controller for propulsion controlled aircraft [microform] : final report (February 1, 1996-January 31, 1997) / prepared by Ping Lu.

    • Text
    • Ames, IA : Dept. of Aerospace Engineering and Engineering Mechanics, Iowa State University ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Low bandwidth robust controllers for flight [microform] : NASA Grant NCC 2-711, June 1991 - December 1992, final report / by Daniel J. Biezad and Hwei-Lan Chou.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • A general fluid system simulation program to model secondary flows in turbomachinery [microform] / Alok K. Majumdar, Katherine P. Van Hooser.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Final technical report for aeroelastic analysis of turbomachinery for space propulsion [microform] : NASA grant number NAG3-1449, grant duration--January 13, 1993 to February 23, 1996 / Theo G. Keith, Jr. & Durbha V. Murthy.

    • Text
    • Toledo, Ohio : Dept. of Mechanical, Industrial and Manufacturing Engineering, University of Toledo ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Shock tunnel studies of scramjet phenomena [microform] : final technical report, NAGW-674.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Performance of low-power pulsed arcjets [microform] : grant no. NASA NAG3-1360 for the period 3/25/93 - 3/24/95 : final report / submitted by Rodney L. Burton.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Preliminary in-flight loads analysis of in-line launch vehicles using the VLOADS 1.4 program [microform] / J.B. Graham and P.L. Luz.

    • Text
    • [Marshall Space Flight Center], Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Model engine performance measurement from force balance instrumentation [microform] / Robert J. Jeracki.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Airfoil dynamic stall and rotorcraft maneuverability [microform] / William G. Bousman.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information, [2000]
    • 2000
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS23428

  • A method of efficient inclination changes for low-thrust spacecraft [microform] / Robert Falck and Leon Gefert ; [prepared for the Astrodynamics Specialist conference and Exhibit ; cosponsored gy the American Institute of Aeronautics and Astronautics and the American Astronautical Society, Monterey, California, August 5-8, 2002].

    • 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/LPS36331

  • High voltage TAL erosion characterization [microform] / David T. Jacobson.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, [2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS59611

  • Low thrust rocket text facility [microform] / Lynn A. Arrington and Steven J. Schneider ; prepared for the 26th Joint Propulsion Conference cosponsored by the AIAA, SAE, ASME, AND ASEE, Orlando, Florida, July 16-18, 1990.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990?]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60608

  • Hybrid propulsion technology program. Volume I, Conceptual design package [microform] : final report / prepared by G. E. Jensen ... [et al.].

    • Text
    • San Jose, CA : United Technologies Chemical Systems ; Marshall Space Flight Center, AL : George C. Marshall Space Flight Center, National Aeronautics and Space Administration, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS68598

  • Hybrid propulsion technology program. Volume II, Technology definition package [microform] / prepared by G. E. Jensen ... [et al.].

    • Text
    • San Jose, CA : United Technologies Chemical Systems ; Marshall Space Flight Center, AL : George C. Marshall Space Flight Center, National Aeronautics and Space Administration, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS68601

  • Centaur D-1A guidance/software system [microform] / Andrew L. Gordan.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984

  • A simulation investigation of the effects of engine- and engine thrust-response characteristics on helicopter handling qualities [microform] / Lloyd D. Corliss and Chris L. Blanken.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; St. Louis, Mo. : United States Army Aviation Research and Development Command, [1983]
    • 1983

  • Docking simulation analysis of range data requirements for the orbital maneuvering vehicle [microform] / by James D. Micheal and Frank L. Vinz.

    • Text
    • [Marshall Space Flight Center, Ala.?] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1985]
    • 1985

  • NASA Fixed Wing Project propulsion research and technology development activities to reduce thrust specific energy consumption / Michael D. Hathaway and Ruben Del Rosario, Nateri K. Madavan.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2013.
    • 2013-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53623

  • Investigation of asymmetric thrust detection with demonstration in a real-time simulation testbed / Amy K. Chicatelli [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2016.
    • 2016-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66959

  • A general fluid system simulation program to model secondary flows in turbomachinery / Alok K. Majumdar, Katherine P. Van Hooser.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1996]
    • 1996
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo79370

  • Airfoil dynamic stall and rotorcraft maneuverability / William G. Bousman.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, July 2000.
    • 2000-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS23428

  • Internal thrust and pumping performance of an auxiliary inlet ejector nozzle with clamshell thrust reverser / by Ali H. Mansour and Richard R. Burley.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, June 1969.
    • 1969-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo189957

No results found from Digital Research Books Beta

Digital books for research from multiple sources world wide- all free to read, download, and keep. No Library Card is Required. Read more about the project.

digital-research-book
Explore Digital Research Books Beta