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  • Characteristics of ions emitted fron high-current hollow cathodes [microform] / by Ikuya Kameyama.

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

  • Operating characteristics of the Russian D-55 thruster with anode layer [microform] / John M. Sankovic and Thomas W. Haag and David H. Manzella.

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

  • SolSTUS [microform] : solar source thermal upper stage.

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

  • A low-erosion starting technique for high-performance arcjets [microform] / John M. Sankovic and Francis M. Curran.

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

  • Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle [microform].

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

  • Metallized gelled propellants [microform] : oxygen/RP-1/aluminum rocket combustion experiments / Bryan Palaszewski and James S. Zakany.

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

  • Performance of a low-power subsonic-arc-attachment arcjet thruster [microform] / John M. Sankovic and Darren H. Berns.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • An analytic approximation to very high specific impulse and specific power interplanetary space mission analysis [microform] / Craig Hamilton Williams.

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

  • Design of a power management and distribution system for a thermionic-diode powered spacecraft [microform] / Greg L. Kimnach.

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

  • Benefits of low-power electrothermal propulsion [microform] / Steven R. Oleson and John M. Sankovic.

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

  • High-power ion thruster technology [microform] / J.R. Beattie and J.N. Matossian.

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

  • Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure [microform] / Robert S. Jankovsky and John M. Kazaroff, Albert J. Pavli.

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

  • Performance of a FAKEL K10K resistojet [microform] / Robert S. Jankovsky and John M. Sankovic, Steven Oleson.

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

  • The diagnostics of the external plasma for the plasma rocket [microform] : final report, NASA Graduate Student Researchers Program, Johnson Space Center, contract number--NGT9-5 / Gerald R. Karr.

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

  • Performance of an axisymmetric rocket based combined cycle engine during rocket only operation using linear regression analysis [microform] / Timothy D. Smith ... [et al.].

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

  • Scaling of ion thrusters to low power [microform] / Michael J. Patterson and Stanley P. Grisnik, George C. Soulas.

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

  • 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

  • Trajectory optimization of an interstellar mission using solar electric propulsion [microform] : final report for NASA grant NAG3-1731 / Craig A. Kluever.

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

  • Analysis of a rocket based combined cycle engine during rocket only operation [microform] / T.D. Smith ... [et al.].

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

  • Advanced low-cost O₂/H₂ engines for the SSTO application [microform] / B. David Goracke and Daniel J.H. Levack, Robert F. Nixon.

    • Text
    • Washington, D.C. : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Mission advantages of constant power, variable ISP electrostatic thrusters [microform] / Steven R. Oleson.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [2000]
    • 2000

  • Performance and endurance tests of a multipropellant resistojet for space station auxiliary propulsion [microform] / W. Earl Morren, Margaret V. Whalen, and James S. Sovey.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
    • 1986

  • Beamed-energy propulsion (BEP) study / Patrick George and Raymond Beach.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo25029

  • Design of a power management and distribution system for a thermionic-diode powered spacecraft / Greg L. Kimnach.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, August 1996.
    • 1996-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70056

  • Benefits of low-power electrothermal propulsion / Steven R. Oleson and John M. Sankovic.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, January 1997.
    • 1997-1
    • 2 Resources

    Available Online

    See All Available Online Resources

  • Ion engine and hall thruster development at the NASA Glenn Research Center / Matthew T. Domonkos, Michael J. Patterson, and Robert S. Jankovsky.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2002.
    • 2002-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS43829

  • Mission advantages of constant power, variable Isp electrostatic thrusters / Steven R. Oleson.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, November 2000.
    • 2000-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo80032

  • Highlights from a Mach 4 experimental demonstration of inlet mode transition for Turbine-Based Combined Cycle hypersonic propulsion / Lancert E. Foster [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo38254

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