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  • The control system for the X-33 linear aerospike engine [microform] / Jerry E. Jackson, Erich Espenschied, Jeffrey Klop.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • A six degree of freedom, plume-fuel optimal trajectory planner for spacecraft proximity operations using an A* node search [microform] / by Mark Charles Jackson.

    • Text
    • Cambridge, Mass. : Charles Stark Draper Laboratory, Inc. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Piloted evaluation of an integrated methodology for propulsion and airframe control design [microform] / Michelle M. Bright ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Adelphi, Md.] : U.S. Army Research Laboratory ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Application of an integrated methodology for propulsion and airframe control design to a STOVL aircraft [microform] / Sanjay Garg and Duane Mattern.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Semi annual progress report for the period June 30, 1988 - December 31, 1988 on the effects of magnetic nozzle configurations on plasma thrusters [microform] / principal investigator, Thomas M. York.

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

  • Digital electronic engine control (DEEC) flight evaluation in an F-15 airplane [microform] : proceedings of a minisymposium held at NASA Ames Research Center, Dryden Flight Research Facility, Edwards, California, May 25-26, 1983.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1984.
    • 1984

  • A vehicle health monitoring system for the space shuttle reaction control system during reentry [microform] / by Anthony David Rosello.

    • Text
    • Cambridge, Mass. : Charles Stark Draper Laboratory ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Design, analysis and control of large transports so that control of engine thrust can be used as a back-up of the primary flight controls [microform] : final technical report, grant #NAG 2-789 / Jan Roskam, principal investigator, Deane E. Ackers.

    • Text
    • Lawrence, Kan. : University of Kansas, Center for Research, Inc. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • An electronic workshop on the performance seeking control and propulsion controlled aircraft results of the F-15 Highly Integrated Digital Electronic Control Flight Research Program [microform] : proceedings of the electronic workshop / compiled by Sheryll Geocke Powers.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor], 1995.
    • 1995

  • Design, analysis, and control of large transport aircraft utilizing selective engine thrust as a backup system for the primary flight control [microform] / Donna S. Gerren.

    • Text
    • [Edwards, Calif.] : National Aeronautics and Space Administration, Dryden Flight Research Facility ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Piloted simulation tests of propulsion control as backup to loss of primary flight controls for a mid-size jet transport [microform] / John Bull ... [et al.].

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

  • The propulsive-only flight control problem [microform] : by Daniel J. Biezad.

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

  • Operational characteristics of the SPT-140 Hall thruster [microform] / David Manzella ... [et al.].

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

  • Pilot-in-the-loop analysis of propulsive-only flight control systems [microform] / by Hwei-Lan Chou, Daniel J. Biezad.

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

  • High stability engine control (HISTEC) flight test results [microform] / Robert D. Southwick ... [et al.].

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

  • Using engine thrust for emergency flight control [microform] : MD-11 and B-747 results / Frank W. Burcham ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Simulator evaluation of simplified propulsion-only emergency flight control systems on transport aircraft [microform] / Frank W. Burcham ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Development and flight test of an emergency flight control system using only engine thrust on an MD-11 transport airplane [microform] / Frank W. Burcham, Jr. ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • A comparison of time-optimal interception trajectories for the F-8 and F-15 [microform] : final report / principal investigator: Anthony J. Calise.

    • Text
    • Atlanta, GA : Georgia Institute of Technology, School of Aerospace Engineering, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69235

  • Numerical analysis of a variable camber rotor blade as a lift cotrol device [microform] / Alfred O. Awani [and] Robert H. Stroub.

    • Text
    • Lawrence, Kans : Flight Research Laboratory, University of Kansas Center for Research, Inc. ; [Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, 1984]
    • 1984

  • Procedure for utilizing the lift and thrust forces of ornithopters [microform] / C. Bezard.

    • Text
    • Washington, DC : National Aeronautics and Space Administration, [1985]
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS98997

  • Voyager Uranus encounter 0.2-lbf T/VA short pulse test report : (final) / prepared by Rocket Research Company ; prepared and approved by D. R. Johnson.

    • Text
    • Pasadena, Calif. : Jet Propulsion Laboratory, California Institute of Technology, [1986]
    • 1986
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS112629

  • Voyager Uranus encounter 0.2-lbf T/VA short pulse test report [microform] : (final) / prepared by Rocket Research Company ; prepared and approved by D. R. Johnson.

    • Text
    • Pasadena, Calif. : Jet Propulsion Laboratory, California Institute of Technology, [1986]
    • 1986

  • An investigation of the use of bandwidth criteria for rotorcraft handling-qualities specifications [microform] / Chris L. Blanken, Courtland C. Bivens, and Matthew S. Whalley.

    • Text
    • Moffett Field, Calif. : Aeromechanics Laboratory, U.S. Army Research and Technology Laboratories (AVSCOM), NASA Ames Research Center, [1985]
    • 1985

  • Polyhedral interpolation for optimal reaction control system jet selection / Leon P. Gefert and Theodore W. Wright.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, June 2014.
    • 2014-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo54247

  • Modeling of commercial turbofan engine with ice crystal ingestion, follow-on / Philip C. E. Jorgenson, Joseph P. Veres, and Ryan Coennen.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2014.
    • 2014-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo57025

  • Development and flight test of an emergency flight control system using only engine thrust on an MD-11 transport airplane / Frank W. Burcham, Jr. [and three others].

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, October 1997.
    • 1997-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo67454

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