Explore: Rocket Nozzles
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Books Results
Source: The Open Library
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Search results from The Open Library
1High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
By Robert S. Jankovsky
“High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation” Metadata:
- Title: ➤ High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
- Author: Robert S. Jankovsky
- Language: English
- Number of Pages: Median: 51
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 1999
- Publish Location: ➤ [Springfield, Va - [Cleveland, Ohio]
“High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation” Subjects and Themes:
- Subjects: ➤ Combustion chambers - Turbulence - Heat transfer - Boundary layer thickness - Heat flux - Rocket nozzles - Flux (Rate) - Pressure distribution - Pressure measurement - Measurement - Transmission - Boundary layer - Rocket engines - Nozzles - Pressure - Heat - Aerodynamic load
Edition Identifiers:
- The Open Library ID: OL17591578M - OL15556459M - OL18137669M - OL20703973M - OL17136005M
- Online Computer Library Center (OCLC) ID: 42885454
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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2Large-displacement structural durability analyses of simple bend specimen emulating rocket nozzle liners
By V. K. Arya
“Large-displacement structural durability analyses of simple bend specimen emulating rocket nozzle liners” Metadata:
- Title: ➤ Large-displacement structural durability analyses of simple bend specimen emulating rocket nozzle liners
- Author: V. K. Arya
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Large-displacement structural durability analyses of simple bend specimen emulating rocket nozzle liners” Subjects and Themes:
- Subjects: ➤ Metal plates - Copper - Elastic bending - Displacement - Thermal fatigue - Rocket linings - Dynamic structural analysis - Rocket nozzles - Fatigue life
Edition Identifiers:
- The Open Library ID: OL15403589M - OL18076259M - OL17113952M
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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3Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure
By M. Moin Hussaini
“Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure” Metadata:
- Title: ➤ Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure
- Author: M. Moin Hussaini
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: Hampton, Va - [Springfield, Va
“Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Rocket nozzles - Low Reynolds number - Nozzle design - Nozzle thrust coefficients - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL15503873M - OL17579534M - OL18121103M
- Online Computer Library Center (OCLC) ID: 40170623
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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4Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure
By Robert S. Jankovsky
“Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure” Metadata:
- Title: ➤ Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure
- Author: Robert S. Jankovsky
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1996
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure” Subjects and Themes:
- Subjects: ➤ Thrust chamber pressure - Exhaust velocity - Divergent nozzles - Specific impulse - Nozzle geometry - Nozzle thrust coefficients - Nozzle efficiency - Rocket nozzles
Edition Identifiers:
- The Open Library ID: OL17126935M - OL17697710M - OL17838890M
- Online Computer Library Center (OCLC) ID: 40386575
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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5Design, 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
Online Access
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6Development of thermal barriers for solid rocket motor nozzle joints
By Bruce M. Steinetz
“Development of thermal barriers for solid rocket motor nozzle joints” Metadata:
- Title: ➤ Development of thermal barriers for solid rocket motor nozzle joints
- Author: Bruce M. Steinetz
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“Development of thermal barriers for solid rocket motor nozzle joints” Subjects and Themes:
- Subjects: ➤ Carbon fibers - Combustion temperature - Fluid flow - High temperature gases - O ring seals - Rocket nozzles - Space shuttle boosters - Thermal insulation
Edition Identifiers:
- The Open Library ID: OL15557193M - OL17591729M
- Online Computer Library Center (OCLC) ID: 42991304
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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7RSRM nozzle fixed housing cooldown test final report
By D. J. Bolieau
“RSRM nozzle fixed housing cooldown test final report” Metadata:
- Title: ➤ RSRM nozzle fixed housing cooldown test final report
- Author: D. J. Bolieau
- Language: English
- Publisher: ➤ Morton Thiokol, Inc., Aerospace Group - National Aeronautics and Space Administration
- Publish Date: 1989
- Publish Location: ➤ Brigham City, Utah - [Washington, D.C
“RSRM nozzle fixed housing cooldown test final report” Subjects and Themes:
- Subjects: Adhesive bonding - Rocket nozzles - Structural analysis - Housings - Space shuttle boosters
Edition Identifiers:
- The Open Library ID: OL17631999M - OL16135465M
- Online Computer Library Center (OCLC) ID: 65287164
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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8Shelf life extension for the lot AAE nozzle severance LSCs
By M. Cook
“Shelf life extension for the lot AAE nozzle severance LSCs” Metadata:
- Title: ➤ Shelf life extension for the lot AAE nozzle severance LSCs
- Author: M. Cook
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, George C. Marshall Space Flight Center? - Thiokol Corp., Space Operations
- Publish Date: 1990
- Publish Location: ➤ Brigham City, UT - [Marshall Space Flight Center, Ala
“Shelf life extension for the lot AAE nozzle severance LSCs” Subjects and Themes:
- Subjects: Exhaust nozzles - Rocket nozzles - Shaped charges - Solid propellant rocket engines - Storage stability
Edition Identifiers:
- The Open Library ID: OL16138451M
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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9A performance comparison of two small rocket nozzles
By Lynn A. Arrington
“A performance comparison of two small rocket nozzles” Metadata:
- Title: ➤ A performance comparison of two small rocket nozzles
- Author: Lynn A. Arrington
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“A performance comparison of two small rocket nozzles” Subjects and Themes:
- Subjects: ➤ Rocket thrust - Thrust chamber pressure - Nozzle design - Reynolds number - Rocket nozzles - Conical nozzles - Film cooling
Edition Identifiers:
- The Open Library ID: OL15452208M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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10Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m(2) (350 psia)
By Tamara A. Smith
“Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m(2) (350 psia)” Metadata:
- Title: ➤ Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m(2) (350 psia)
- Author: Tamara A. Smith
- Number of Pages: Median: 21
- Publisher: Lewis Research Center
- Publish Date: 1987
- Publish Location: Cleveland, Ohio
“Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m(2) (350 psia)” Subjects and Themes:
- Subjects: Rocket nozzles - Nozzle design
Edition Identifiers:
- The Open Library ID: OL19003685M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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11Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20
By George T. Carson
“Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20” Metadata:
- Title: ➤ Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20
- Author: George T. Carson
- Language: English
- Number of Pages: Median: 171
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Division
- Publish Date: 1988
- Publish Location: ➤ Springfield, Va - [Washington, D.C.]
“Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20” Subjects and Themes:
- Subjects: ➤ Ramjet engines - Nozzle efficiency - Turbine engines - Jet nozzles - Rocket nozzles - Nozzle geometry - Mach number
Edition Identifiers:
- The Open Library ID: OL16116426M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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12Advanced small rocket chambers option 3
By Donald M. Jassowski
“Advanced small rocket chambers option 3” Metadata:
- Title: ➤ Advanced small rocket chambers option 3
- Author: Donald M. Jassowski
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Advanced small rocket chambers option 3” Subjects and Themes:
- Subjects: ➤ Thermal cycling tests - Mechanical engineering - Design analysis - Engine tests - Iridium - Thrust chambers - Combustion chambers - Aerospace engineering - Rocket nozzles - Thermal analysis - Rhenium - Engine design - Harmonic analysis - Weld tests - Metal coatings - Performance tests - Dynamic structural analysis - Nozzle design - Computer aided design
Edition Identifiers:
- The Open Library ID: OL15419293M
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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13Comparison of response surface and kriging models in the multidisciplinary design of an aerospike nozzle
By Timothy W. Simpson
“Comparison of response surface and kriging models in the multidisciplinary design of an aerospike nozzle” Metadata:
- Title: ➤ Comparison of response surface and kriging models in the multidisciplinary design of an aerospike nozzle
- Author: Timothy W. Simpson
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering, NASA Langley Research Center
- Publish Date: 1998
- Publish Location: Hampton, VA - Springfield, VA
“Comparison of response surface and kriging models in the multidisciplinary design of an aerospike nozzle” Subjects and Themes:
- Subjects: ➤ Aerospike engines - Kriging - Rocket nozzles - Propulsion system configurations - Multidisciplinary design optimization - Design analysis
Edition Identifiers:
- The Open Library ID: OL15547305M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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14A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center
By Kenneth J. Davidian
“A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center” Metadata:
- Title: ➤ A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center
- Author: Kenneth J. Davidian
- Language: English
- Number of Pages: Median: 28
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1987
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.?]
“A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center” Subjects and Themes:
- Subjects: ➤ Nozzles - Rockets (Aeronautics) - Rocket nozzles - Nozzle geometry - High aspect ratio - Research facilities
Edition Identifiers:
- The Open Library ID: OL15419235M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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15Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle
By Kenneth J. Kacynski
“Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle” Metadata:
- Title: ➤ Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle
- Author: Kenneth J. Kacynski
- Number of Pages: Median: 24
- Publisher: Lewis Research Center
- Publish Date: 1987
- Publish Location: Cleveland, Ohio
“Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle” Subjects and Themes:
- Subjects: Rocket nozzles - Heat flux - Nozzle design
Edition Identifiers:
- The Open Library ID: OL22344658M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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16Flight motor set 360L002 (STS-27R)
By S. A. Meyer
“Flight motor set 360L002 (STS-27R)” Metadata:
- Title: ➤ Flight motor set 360L002 (STS-27R)
- Author: S. A. Meyer
- Language: English
- Publisher: ➤ Thiokol Corp., Space Operations - National Aeronautics and Space Administration, George C. Marshall Space Flight Center
- Publish Date: 1989
- Publish Location: ➤ Marshall Space Flight Center, Ala - Brigham City, UT
“Flight motor set 360L002 (STS-27R)” Subjects and Themes:
- Subjects: ➤ Performance tests - Postmission analysis (Spacecraft) - Propulsion systems - Rocket nozzles - Space shuttles - Postflight analysis - Solid propellant rocket engines
Edition Identifiers:
- The Open Library ID: OL16138448M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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