Explore: Hydrogen Oxygen Engines
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Source: The Open Library
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1Fiber-reinforced ceramic composites for Earth-to-orbit rocket engine turbines
By Jerry W. Brockmeyer
“Fiber-reinforced ceramic composites for Earth-to-orbit rocket engine turbines” Metadata:
- Title: ➤ Fiber-reinforced ceramic composites for Earth-to-orbit rocket engine turbines
- Author: Jerry W. Brockmeyer
- Language: English
- Publisher: ➤ Rocketdyne Division, Rockwell International - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1990
- Publish Location: ➤ Cleveland. Ohio - Canoga Park, CA
“Fiber-reinforced ceramic composites for Earth-to-orbit rocket engine turbines” Subjects and Themes:
- Subjects: ➤ Space transportation - Turbine pumps - Silicon carbides - Ceramic matrix composites - Fiber composites - Hydrogen oxygen engines - Rotors - Turbine blades
Edition Identifiers:
- The Open Library ID: OL18263308M - OL16138410M - OL17632391M
- Online Computer Library Center (OCLC) ID: 68810201
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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27.5K lbf thrust engine preliminary design for orbit transfer vehicle
By Warren R. Hayden
“7.5K lbf thrust engine preliminary design for orbit transfer vehicle” Metadata:
- Title: ➤ 7.5K lbf thrust engine preliminary design for orbit transfer vehicle
- Author: Warren R. Hayden
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“7.5K lbf thrust engine preliminary design for orbit transfer vehicle” Subjects and Themes:
- Subjects: Hydrogen oxygen engines - Rocket engine design - Turbine pumps - Spacecraft propulsion - Orbit transfer vehicles
Edition Identifiers:
- The Open Library ID: OL14667916M - OL15402007M - OL18075584M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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3Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle
By R. W. Marable
“Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle” Metadata:
- Title: ➤ Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle
- Author: R. W. Marable
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Pratt and Whitney Aircraft
- Publish Date: 1989
- Publish Location: ➤ Springfield, Va - [West Palm Beach, Fla - Washington, DC
“Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle” Subjects and Themes:
- Subjects: ➤ RL-10 engines - Specific impulse - Propulsion system performance - Performance tests - Engine tests - Hydrogen oxygen engines - Combustion chambers - Reusable rocket engines - Rocket nozzles - Nozzle design - Rocket engine design - Fabrication
Edition Identifiers:
- The Open Library ID: OL15407985M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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4A comparison of analytical results for 20 K LOX/hydrogen instabilities
By Mark D. Klem
“A comparison of analytical results for 20 K LOX/hydrogen instabilities” Metadata:
- Title: ➤ A comparison of analytical results for 20 K LOX/hydrogen instabilities
- Author: Mark D. Klem
- Language: English
- Number of Pages: Median: 15
- Publisher: ➤ NASA - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“A comparison of analytical results for 20 K LOX/hydrogen instabilities” Subjects and Themes:
- Subjects: ➤ Computer simulation - Combustion - Liquid propellants - Liquid propellant rockets - Combustion stability - Fuel injection - Rocket engines - Hydrogen oxygen engines - Computer programs
Edition Identifiers:
- The Open Library ID: OL16123553M - OL17634485M
- Online Computer Library Center (OCLC) ID: 25023352
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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5A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis
By Kenneth John Kacynski
“A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis” Metadata:
- Title: ➤ A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis
- Author: Kenneth John Kacynski
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1991
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis” Subjects and Themes:
- Subjects: ➤ Engine coolants - Heat transfer - Heat exchangers - Combustion chambers - Cooling systems - Hydrogen oxygen engines - Rocket engines
Edition Identifiers:
- The Open Library ID: OL18072965M - OL15399333M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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6Dual-throat thruster thermal model
By R. L. Ewen
“Dual-throat thruster thermal model” Metadata:
- Title: ➤ Dual-throat thruster thermal model
- Author: R. L. Ewen
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Marshall Space Flight Center, Alabama - Aerojet TechSystems Co. - National Technical Information Service, distributor
- Publish Date: 1986
- Publish Location: ➤ [Springfield, Va - [Huntsville, Ala.] - Sacramento, Calif
“Dual-throat thruster thermal model” Subjects and Themes:
- Subjects: ➤ Hydrogen oxygen engines - Engine design - Dual thrust nozzles - Nozzle design - Spacecraft propulsion - Combustion chambers
Edition Identifiers:
- The Open Library ID: OL18082798M - OL15416488M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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7Reduced H2-O2 mechanisms for use in reacting flow simulation
By B. D. Hitch
“Reduced H2-O2 mechanisms for use in reacting flow simulation” Metadata:
- Title: ➤ Reduced H2-O2 mechanisms for use in reacting flow simulation
- Author: B. D. Hitch
- Number of Pages: Median: 10
- Publisher: AIAA
- Publish Date: 1988
- Publish Location: New York
“Reduced H2-O2 mechanisms for use in reacting flow simulation” Subjects and Themes:
- Subjects: ➤ Hydrogen oxygen engines - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL18926367M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios
By Kenneth John Kacynski
“The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios” Metadata:
- Title: ➤ The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios
- Author: Kenneth John Kacynski
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios” Subjects and Themes:
- Subjects: ➤ Heat transfer - Thermal diffusion - Nozzle flow - Sweat cooling - Film cooling - Hydrogen oxygen engines - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15404461M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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9Qualitative flow visualization of a 110-N hydrogen/oxygen laboratory model thruster
By Wim A. de Groot
“Qualitative flow visualization of a 110-N hydrogen/oxygen laboratory model thruster” Metadata:
- Title: ➤ Qualitative flow visualization of a 110-N hydrogen/oxygen laboratory model thruster
- Author: Wim A. de Groot
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1997
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“Qualitative flow visualization of a 110-N hydrogen/oxygen laboratory model thruster” Subjects and Themes:
- Subjects: ➤ Two dimensional models - Altitude simulation - Emission spectra - Raman spectra - Hydrogen oxygen engines - High altitude - Combustion chambers - Flow visualization - Ultraviolet spectroscopy - Thrustors
Edition Identifiers:
- The Open Library ID: OL15539871M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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10A unique high heat flux facility for testing hypersonic engine components
By Matthew E. Melis
“A unique high heat flux facility for testing hypersonic engine components” Metadata:
- Title: ➤ A unique high heat flux facility for testing hypersonic engine components
- Author: Matthew E. Melis
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1990
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“A unique high heat flux facility for testing hypersonic engine components” Subjects and Themes:
- Subjects: ➤ Engine parts - Test facilities - Heat flux - Cooling - Hypersonic vehicles - Hydrogen oxygen engines
Edition Identifiers:
- The Open Library ID: OL15405890M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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11A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis
By Kenneth J. Kacynski
“A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis” Metadata:
- Title: ➤ A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis
- Author: Kenneth J. Kacynski
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1991
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis” Subjects and Themes:
- Subjects: ➤ Engine coolants - Heat transfer - Heat exchangers - Combustion chambers - Cooling systems - Hydrogen oxygen engines - Rocket engines
Edition Identifiers:
- The Open Library ID: OL17113180M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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12Predicted performance of an integrated modular engine system
By Michael P. Binder
“Predicted performance of an integrated modular engine system” Metadata:
- Title: ➤ Predicted performance of an integrated modular engine system
- Author: Michael P. Binder
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1993
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Predicted performance of an integrated modular engine system” Subjects and Themes:
- Subjects: ➤ Modularity - Propulsion system performance - Spacecraft propulsion - Propulsion system configurations - Hydrogen oxygen engines - Performance prediction - Rocket engine design - Fault tolerance
Edition Identifiers:
- The Open Library ID: OL15411266M
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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13A transient model of the RL10A-3-3A rocket engine
By Michael P. Binder
“A transient model of the RL10A-3-3A rocket engine” Metadata:
- Title: ➤ A transient model of the RL10A-3-3A rocket engine
- Author: Michael P. Binder
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“A transient model of the RL10A-3-3A rocket engine” Subjects and Themes:
- Subjects: ➤ Engine design - Rocket launching - Centaur launch vehicle - Propulsion system configurations - Engine tests - Hydrogen oxygen engines - Computer aided design - Mathematical models - Rocket engine design - Aerospace engineering
Edition Identifiers:
- The Open Library ID: OL15414605M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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14Highly Evolved Expendable Launch Vehicle (HEELV) for the HRST program
“Highly Evolved Expendable Launch Vehicle (HEELV) for the HRST program” Metadata:
- Title: ➤ Highly Evolved Expendable Launch Vehicle (HEELV) for the HRST program
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Highly Evolved Expendable Launch Vehicle (HEELV) for the HRST program” Subjects and Themes:
- Subjects: ➤ Launch costs - Expendable stages (Spacecraft) - Engine design - Launch vehicles - Spacecraft launching - Hydrogen oxygen engines - Low earth orbits - Thrust-weight ratio - Low cost
Edition Identifiers:
- The Open Library ID: OL17831289M
- Online Computer Library Center (OCLC) ID: 39491050
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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