Search results for: Kacynski, Kenneth J.
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1
Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle
Authors: Kacynski, Kenneth J.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1987Physical Description: 1 volume.Holdings: Loading…
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2
Thermal stratification potential in rocket engine coolant channels
Authors: Kacynski, Kenneth J.
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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3
A three-dimensional turbulent heat transfer analysis for advanced tubular rocket thrust chambers
Authors: Kacynski, Kenneth J.
Published: National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1990Physical Description: 1 volume.Holdings: Loading…
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4
A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis
Authors: Kacynski, Kenneth J.
Published: National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1991Physical Description: 1 volume.Holdings: Loading…
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5
The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios
Authors: Kacynski, Kenneth J.
Published: National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1994Physical Description: 1 volume.Holdings: Loading…
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6
Analytical study of nozzle performance for nuclear thermal rockets
Authors: Davidian, Kenneth O.Other Authors: “…Kacynski, Kenneth J.…”
Published: National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1991
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7
Nuclear thermal rocket nozzle testing and evaluation program
Authors: Davidian, Kenneth O.Other Authors: “…Kacynski, Kenneth J.…”
Published: [National Aeronautics and Space Administration] ; [For sale by the National Technical Information Service], 1993
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8
Experimental thrust performance of a high-area-ratio rocket nozzle
Authors: Pavli, Albert J.Other Authors: “…Kacynski, Kenneth J.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1987
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9
Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m.
Authors: Smith, Tamara A.Other Authors:
Published: National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1987Physical Description: 1 volume.Holdings: Loading…
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Related Subjects
Nozzles
Rocket engines
Rockets (Aeronautics)
HEAT TRANSFER
Heat
Hydrogen oxygen engines
Nuclear rockets
Transmission
Combustion chambers
Computer simulation
Cooling
Cooling systems
Engine coolants
Film cooling
Flow distribution
Heat exchangers
Nozzle flow
Nuclear propulsion
Sweat cooling
Thermal diffusion
Thrust