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7.5K lbf thrust engine preliminary design for orbit transfer vehicle [microform] : task D.5 final report / Warren R. Hayden, Ralph Sabiers, and Judy Schneider.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
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
0 resources
Recycle requirements for NASA's 30cm xenon ion thruster [microform] / Luis R. Piñero and Vincent K. Rawlin.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Integrated propulsion technology demonstrator program plan [microform] : program plan.
Text
[Marshall Space Flight Center, Ala.] : Marshall Space Flight Center ; [Downey, Calif.] : Rockwell Aerospace ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Nuclear thermal propulsion [microform] : a joint NASA/DOE/DOD Workshop : proceedings of the Nuclear Thermal Propulsion Workshop held at the Holiday Inn Strongsville, Ohio.
Text
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1991.
1991
0 resources
Developments in REDES [microform] : the rocket engine design expert system / Kenneth O. Davidian.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
1990
0 resources
Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle [microform].
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[West Palm Beach, Fla. : Pratt and Whitney Aircraft ; Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
1989
0 resources
"Fast Track" NTR systems assessment for NASA's first lunar outpost scenario [microform] / Stanley K. Borowski and Stephen W. Alexander.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
1992
0 resources
Engine system assessment study using Martian propellants [microform] : final report / prepared by Dennis Pelaccio ... [et al.].
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Torrance, CA : Science Applications International Corp. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
1992
0 resources
Arcjet thruster research and technology [microform] : phase II final report, NAS 3-24631 / prepared by Rocket Research Company.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1991]
1991
0 resources
Program test objectives milestone 3 [microform] / T.L. Gaynor, principal investigator.
Text
[Huntsville, Ala.] : Marshall Space Flight Center ; [Downey, Calif.] : Rockwell Aerospace, Space Systems Division ; Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
High performance storable propellant resistojet [microform] : final report.
Text
Cleveland, OH : NASA Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
1992
0 resources
Advanced small rocket chambers option II [microform] : fundamental processes and material evaluation : final report / Donald M. Jassowski.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
1993
0 resources
Predicted performance of an integrated modular engine system [microform] / Michael Binder and James L. Felder.
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
1993
0 resources
Arcjet thruster research and technology [microform] : final report / prepared by Darby B. Makel, Gordon L. Cann.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]
1988
0 resources
Orbit transfer rocket engine technology program [microform] : interim report : advanced engine study, task D.1/D.3 / prepared by A. Martinez, C. Erickson, B. Hines.
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Canoga Park, CA : Rocketdyne Division of Rockwell International Corporation ; [Washington, D.C. : National Aeronautics and Space Administration : Springfield, Va. : National Technical Informaiton Service, distributor, 1986]
1986
0 resources
Propellant injection systems and processes [microform] / Jackson I. Ito.
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[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Advanced Earth-to-orbit propulsion technology information, dissemination, and research [microform] : final report ... July 28, 1993 - March 28, 1995 / prepared by S.T. Wu.
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[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Solid-propellant rocket motor internal ballistics performance variatio analysis (phase five) [microform] : final report / by Richard H. Sforzini and Jesse E. Murph.
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Auburn, Ala. : Engineering Experiment Station, Auburn University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1980]
1980
0 resources
Space Transportation Booster Engine (STBE) configuration study [microform] : second quarterly review.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
1986
0 resources
Electrically heated tube investigation of cooling channel geometry effects [microform] / Michael L. Meyer.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Robust rocket engine concept [microform] / Carl F. Lorenzo.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
A transient model of the RL10A-3-3A rocket engine [microform] / Michael P. Binder.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
BSM Delta qualification 2 [microform] : final report / prepared by United Technologies Chemical Systems.
Text
San Jose, Calif. : The Systems ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Micro electric propulsion feasibility [microform] / Graeme Aston and Martha Aston.
Text
[Washington, D.C.] : NASA ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
1992
0 resources
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
0 resources
Redesign and test of an SSME turbopump for the Large Throat Main Combustion Chamber [microform] / K.J. Lunde ... [et al.].
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Rocket-based combined cycle engine technology development [microform] : inlet CFD validation and application / J.R. DeBonis and S. Yungster.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Aeronautics and Space Administration, distributor], 1996.
1996
0 resources
Preliminary evaluation of a 10 kW Hall thruster [microform] / Robert S. Jankovsky, Chris McLean and John McVey.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
Experimental evaluation of a subscale gaseous hydrogen/gaseous oxygen coaxial rocket injector [microform] / Timothy D. Smith ... [et al.].
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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/LPS43891The effect of cooling passage aspect ratio on curvature heat transfer enhancement [microform] / Michael L. Meyer.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS53769Orbital transfer vehicle oxygen turbopump technology. Volume I, Design, fabrication, and hydrostatic bearing testing [microform] : final report / P.S. Buckmann, ... [et al.].
Text
[Washington, D.C.] : National Aeronautics and Space Administration, [1990]
1990
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS60999Second Magnetoplasmadynamic Thruster Workshop [microform] : proceedings of a workshop sponsored by and held at NASA Lewis Research Center, May 19, 1992.
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[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
1992
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS66962SRB thermal curtain design support [microform] : October 1990 interim report to U.S. Polymeric, B.P. Chemicals / prepared by Wayne E. Lundblad.
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Birmingham, Ala. : Southern Research Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1990]
1990
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS69365Air intakes for a probative missile of rocket ramjet [microform] / G. Laruelle.
Text
Washington, D.C. : National Aeronautics and Space Administration, [1984]
1984
0 resources
NASA's chemical transfer propulsion program for Pathfinder / Ned P. Hannum and Frank D. Berkopec, and Robert L. Zurawski.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, [1989]
1989
1 resource
Available online
https://purl.fdlp.gov/GPO/LPS108054NASA's chemical transfer propulsion program for Pathfinder [microform] / Ned P. Hannum and Frank D. Berkopec, and Robert L. Zurawski.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, [1989]
1989
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS108054Arcjet thruster research and technology [microform] : phase I final report / [prepared by Seven C. Knowles].
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Cleveland, OH : NASA Lewis Research Center, [1987]
1987
0 resources
Orbital transfer vehicle engine integration study [microform] : final report / prepared by W.J. Ketchum.
Text
San Diego, Calif. : Advanced Space Programs, General Dynamics Convair Division ; [Washington, D.C. : National Aeronautics and Space Administration?, 1984]
1984
0 resources
Design and analysis report for the RL10-2B breadboard low thrust engine [microform] : final report / James R. Brown ... et al. ; prepared by United Technologies Corporation, Pratt & Whitney ; prepared for National Aeronautics and Space Administration, Lewis Research Center.
Text
West Palm Beach, FL. : United Technologies Corporation, Pratt & Whitney, Government Products Division, [1984]
1984
0 resources
Rocket-based combined cycle engine technology development : inlet CFD validation and application / J.R. DeBonis and S. Yungster.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, June 1996.
1996-6
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo69485Experimental evaluation of a subscale gaseous hydrogen/gaseous oxygen coaxial rocket injector / Timothy D. Smith [and four others].
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, November 2002.
2002-11
1 resource
Available online
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