Search results for: Arrington, Lynn A.
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1
A performance comparison of two small rocket nozzles
Authors: Arrington, Lynn A.
Published: National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1996Physical Description: 1 volume.Holdings: Loading…
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2
Multi-axis thrust measurements of the EO-1 pulsed plasma thruster
Authors: Arrington, Lynn A.
Published: National Aeronautics and Space Administration, Glenn Research Center ; [National Technical Information Service, distributor], 1999Physical Description: 1 volume.Holdings: Loading…
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3
Low thrust rocket text facility
Authors: Arrington, Lynn A.
Published: NASA ; [For sale by the National Technical Information Service], 1990Physical Description: 20 pages : illustrations., Also available via Internet from the NASA Technical Report Server web site. Address as of 5/18/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900015842%5F1990015842.pdf; current access available via PURL.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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4
Performance comparison of axisymmetric and three-dimensional hydrogen film coolant injection in a 110N hydrogen/oxyen rocket
Authors: Arrington, Lynn A.
Published: National Aeronautics and Space Administration, Lewis Research Center, 1992Physical Description: 1 online resource (20 pages) : digital, PDF file.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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5
A performance comparison of pulsed plasma thruster electrode configurations
Authors: Arrington, Lynn A.
Published: National Aeronautics and Space Administration, Lewis Research Center, 1997Physical Description: 1 online resource (8 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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6
Multi-axis thrust measurements of the EO-1 pulsed plasma thruster
Authors: Arrington, Lynn A., Haag, Thomas W.
Published: National Aeronautics and Space Administration, Glenn Research Center, 1999Physical Description: 1 online resource (16 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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7
A performance comparison of two small rocket nozzles
Authors: Arrington, Lynn A., Reed, Brian D., Rivera, Angel
Published: National Aeronautics and Space Administration, Lewis Research Center, 1996Physical Description: 1 online resource (11 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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8
A performance comparison of pulsed plasma thruster electrode configurations
Published: National Aeronautics and Space Administration, Lewis Research Center ; [National Technical Information Service, distributor], 1997Other Authors: “…Arrington, Lynn A.…”
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Related Subjects
Rocket thrust
Film cooling
Low thrust
Propulsion system performance
Conical nozzles
Low thrust propulsion
Nozzle design
Performance tests
Plasma electrodes
Plasma engines
Pulse charging
Pulsed jet engines
Reynolds number
Rocket engines
Rocket nozzles
Thrust chamber pressure
Axisymmetric flow
Chemical propulsion
Coolants
Fluid injection
Hydrogen
Hydrogen oxygen engines
Nondestructive tests
Reacting flow
Reaction kinetics
Rocket test facilities
Rockets (Aeronautics)
Testing
Three dimensional flow
Thrust