Search Results - Arrington, Lynn A.
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1
Multi-axis thrust measurements of the EO-1 pulsed plasma thruster by Arrington, Lynn A.
Published 1999Call Number: Loading…
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2
A performance comparison of pulsed plasma thruster electrode configurations / by Arrington, Lynn A.
Published 1997Call Number: Loading…Online Access
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3
Low thrust rocket text facility by Arrington, Lynn A.
Published 1990Call Number: Loading…Connect to online resource
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4
A performance comparison of two small rocket nozzles by Arrington, Lynn A.
Published 1996Call Number: Loading…
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5
Performance comparison of axisymmetric and three-dimensional hydrogen film coolant injection in a 110N hydrogen/oxyen rocket by Arrington, Lynn A.
Published 1992Call Number: Loading…Online Access
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6
Multi-axis thrust measurements of the EO-1 pulsed plasma thruster / by Arrington, Lynn A., Haag, Thomas W.
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7
A performance comparison of two small rocket nozzles / by Arrington, Lynn A., Reed, Brian D., Rivera, Angel
Published 1996Call Number: Loading…Online Access
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8
A performance comparison of pulsed plasma thruster electrode configurations
Published 1997Other Authors: “…Arrington, Lynn A.…”
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Related Subjects
Rocket thrust
Film cooling
Propulsion system performance
Conical nozzles
Low thrust
Low thrust propulsion
Nozzle design
Performance tests
Plasma electrodes
Plasma engines
Pulse charging
Pulsed jet engines
Reynolds number
Rocket engines
Rocket nozzles
Rockets (Aeronautics)
Thrust chamber pressure
Axisymmetric flow
Coolants
Fluid injection
Hydrogen
Hydrogen oxygen engines
Nozzles
Reacting flow
Testing
Three dimensional flow