Explore: Propellant Combustion
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Books Results
Source: The Open Library
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Search results from The Open Library
1Fuel-rich catalytic combustion of a high density fuel
By Theodore A. Brabbs
“Fuel-rich catalytic combustion of a high density fuel” Metadata:
- Title: ➤ Fuel-rich catalytic combustion of a high density fuel
- Author: Theodore A. Brabbs
- Language: English
- Number of Pages: Median: 11
- Publisher: ➤ For sale by the National Technical Information Service - Lewis Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1993
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va - Cleveland, Ohio
“Fuel-rich catalytic combustion of a high density fuel” Subjects and Themes:
- Subjects: ➤ Fuel combustion - Hydrocarbon combustion - Propellant combustion - Supersonic combustion - Hydrocarbon fuels - Combustion control - Combustion products - Catalysis - Catalytic combustion
Edition Identifiers:
- The Open Library ID: OL16125621M - OL19146774M - OL18227608M - OL19916521M
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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2Metallized gelled propellants
By Bryan A. Palaszewski
“Metallized gelled propellants” Metadata:
- Title: Metallized gelled propellants
- Author: Bryan A. Palaszewski
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995 - 1996 - 1997
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va - [Washington, D.C - Springfield, Va
“Metallized gelled propellants” Subjects and Themes:
- Subjects: ➤ Heat flux - Heat transfer - Metal combustion - Liquid rocket propellants - Rocket engines - Gelled propellants - Metal propellants - Propellant combustion - Propellant additives - Flux quantization - Aluminum - Hydrocarbon fuels - Specific impulse - Temperature profiles - Gelled rocket propellants - Oxygen - Calorimeters - Propulsive efficiency - Propulsion system performance - Heat measurement
Edition Identifiers:
- The Open Library ID: OL17131208M - OL17125103M - OL15420743M
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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The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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3Testing of wrought iridium/chemical vapor deposition rhenium rocket
By Brian D. Reed
“Testing of wrought iridium/chemical vapor deposition rhenium rocket” Metadata:
- Title: ➤ Testing of wrought iridium/chemical vapor deposition rhenium rocket
- Author: Brian D. Reed
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Testing of wrought iridium/chemical vapor deposition rhenium rocket” Subjects and Themes:
- Subjects: ➤ Propellant combustion - Wrought alloys - Rhenium - Oxygen - Iridium - Combustion temperature - Vapor deposition - Storable propellants - Linings - Hydrogen
Edition Identifiers:
- The Open Library ID: OL17837240M - OL15497596M
- Online Computer Library Center (OCLC) ID: 39854969
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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4Turbine engine hot section technology 1986
By Lewis Research Center
“Turbine engine hot section technology 1986” Metadata:
- Title: ➤ Turbine engine hot section technology 1986
- Author: Lewis Research Center
- Language: English
- Number of Pages: Median: 503
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: [Washington, D.C.]
“Turbine engine hot section technology 1986” Subjects and Themes:
- Subjects: ➤ Propellant combustion - Heat transfer - Thermal control coatings - Transmission - High temperatures - Fatigue (Materials) - Gas turbine engines - Materials - Structural analysis - Fatigue - Conferences - Fracture mechanics - Heat - Congresses - Measuring instruments - Aircraft gas-turbines
Edition Identifiers:
- The Open Library ID: OL14544621M
- Online Computer Library Center (OCLC) ID: 27459800
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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5Propellant injection systems and processes
By Jackson I. Ito
“Propellant injection systems and processes” Metadata:
- Title: ➤ Propellant injection systems and processes
- Author: Jackson I. Ito
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Propellant injection systems and processes” Subjects and Themes:
- Subjects: ➤ Propellant combustion - Liquid injection - Fuel injection - Injectors - Rocket engine design - Liquid rocket propellants
Edition Identifiers:
- The Open Library ID: OL15413556M
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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6Hybrid fuel formulation and technology development
By David L. Dean
“Hybrid fuel formulation and technology development” Metadata:
- Title: ➤ Hybrid fuel formulation and technology development
- Author: David L. Dean
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - McDonnell Douglas
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC] - Huntsville, AL
“Hybrid fuel formulation and technology development” Subjects and Themes:
- Subjects: ➤ Propellant combustion - Hybrid propellants - Propellant grains - Hydrocarbon fuels - Propellant tests - Propellant properties - Fuel tests
Edition Identifiers:
- The Open Library ID: OL15419693M
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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7Carbon monoxide and oxygen combustion experiments
By Diane L. Linne
“Carbon monoxide and oxygen combustion experiments” Metadata:
- Title: ➤ Carbon monoxide and oxygen combustion experiments
- Author: Diane L. Linne
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1991
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Carbon monoxide and oxygen combustion experiments” Subjects and Themes:
- Subjects: ➤ Liquid propellant rocket engines - Propellant combustion - Liquid oxygen - Carbon monoxide - Propulsion system performance - Spacecraft propulsion - Liquid rocket propellants
Edition Identifiers:
- The Open Library ID: OL15399332M
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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8Round robin results of the closed bomb and strand burner
By Arpad A. Juhasz
“Round robin results of the closed bomb and strand burner” Metadata:
- Title: ➤ Round robin results of the closed bomb and strand burner
- Author: Arpad A. Juhasz
- Publisher: ➤ Chemical Propulsion Information Agency, Johns Hopkins University, Applied Physics Laboratory
- Publish Date: 1982
- Publish Location: Laurel, Md
“Round robin results of the closed bomb and strand burner” Subjects and Themes:
- Subjects: Propellant combustion - Closed bomb - Burning rate - Strand burner
Edition Identifiers:
- The Open Library ID: OL20268932M
Access and General Info:
- First Year Published: 1982
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9Long life testing of oxide-coated iridium/rhenium rockets
By Brian D. Reed
“Long life testing of oxide-coated iridium/rhenium rockets” Metadata:
- Title: ➤ Long life testing of oxide-coated iridium/rhenium rockets
- Author: Brian D. Reed
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Long life testing of oxide-coated iridium/rhenium rockets” Subjects and Themes:
- Subjects: ➤ Propellant combustion - Refractory metals - Materials tests - Ceramic coatings - Oxidation - Iridium - Rhenium - Performance tests - Protective coatings - Combustion chambers - Radiant cooling - Substrates - Service life
Edition Identifiers:
- The Open Library ID: OL15421602M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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10Questions of testing rate and flexibility of rocket test benches
By Legrand.
“Questions of testing rate and flexibility of rocket test benches” Metadata:
- Title: ➤ Questions of testing rate and flexibility of rocket test benches
- Author: Legrand.
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Leo Kanner Associates]
- Publish Date: 1987
- Publish Location: ➤ Washington, D.C - [Springfield, Va - [Redwood City, Calif
“Questions of testing rate and flexibility of rocket test benches” Subjects and Themes:
- Subjects: Propellant combustion - Test stands - Burning rate - Rocket test facilities
Edition Identifiers:
- The Open Library ID: OL16054884M
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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11Thruster injector faceplate testing in support of the aerojet Rocket-based combined cycle (RBCC) concept
By M. M. Fazah
“Thruster injector faceplate testing in support of the aerojet Rocket-based combined cycle (RBCC) concept” Metadata:
- Title: ➤ Thruster injector faceplate testing in support of the aerojet Rocket-based combined cycle (RBCC) concept
- Author: M. M. Fazah
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Marshall Space Flight Center
- Publish Date: 1998
- Publish Location: ➤ [Marshall Space Flight Center, Ala.] - [Springfield, Va
“Thruster injector faceplate testing in support of the aerojet Rocket-based combined cycle (RBCC) concept” Subjects and Themes:
- Subjects: ➤ Rocket firing - Propellant combustion - Test firing - Hydrogen fuels - Injectors - Firing (Igniting) - Rocket engines - Engine tests - Fuel combustion - Gas-gas interactions
Edition Identifiers:
- The Open Library ID: OL15541902M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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