Search results for: Kazaroff, John M.
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1
Conventionally cast and forged copper alloy for high-heat-flux thrust chambers
Authors: Kazaroff, John M.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1987Physical Description: 1 volume.Holdings: Loading…
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2
New method of making advanced tube-bundle rocket thrust chambers
Authors: Kazaroff, John M.
Published: National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1990Physical Description: 1 volume.Holdings: Loading…
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3
Cyclic hot firing of tungsten-wire-reinforced, copper-lined thrust chambers
Authors: Kazaroff, John M.
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1990Physical Description: 1 volume.Holdings: Loading…
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4
Hot fire test results of subscale tubular combustion chambers
Authors: Kazaroff, John M.
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1992Physical Description: 1 volume.Holdings: Loading…
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5
Advanced tube-bundle rocket thrust chamber
Authors: Kazaroff, John M.
Published: NASA ; [For sale by the National Technical Information Service], 1990Physical Description: 12 pages : illustrations., Also available via Internet from the NASA Technical Report Server web site. Address as of 4/15/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900015869%5F1990015869.pdf; current access available via PURL.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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6
Iridium-coated rhenium thrusters by CVD
Authors: Harding, John T.Other Authors: “…Kazaroff, John M.…”
Published: National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1988
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7
Hot fire fatigue testing results for the compliant combustion chamber
Authors: Pavli, Albert J.Other Authors: “…Kazaroff, John M.…”
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1992
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8
A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis
Authors: Kacynski, Kenneth J.Other Authors: “…Kazaroff, John M.…”
Published: National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1991
Physical Description: 1 volume.Holdings: Loading…
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9
Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure
Authors: Jankovsky, Robert S.Other Authors: “…Kazaroff, John M.…”
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1996
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Related Subjects
Rocket engines
Combustion chambers
Thrust
Fatigue
Materials
Cooling systems
Copper alloys
Divergent nozzles
Engine coolants
Exhaust velocity
HEAT TRANSFER
Heat exchangers
Hydrogen oxygen engines
Iridium
Life (Durability)
Metallography
Metallurgy
Nozzle efficiency
Nozzle geometry
Nozzle thrust coefficients
Propulsion systems
Rhenium
Rocket nozzles
Rocket thrust
Rockets (Aeronautics)
Space vehicles
Specific impulse
Thrust chamber pressure
Thrust chambers
Weight reduction