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Source: The Open Library
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Search results from The Open Library
1High-power ion thruster technology
By J. R. Beattie
“High-power ion thruster technology” Metadata:
- Title: ➤ High-power ion thruster technology
- Author: J. R. Beattie
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1992 - 1996
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“High-power ion thruster technology” Subjects and Themes:
- Subjects: ➤ Charge transfer - Ion propulsion - Plasma propulsion - Pressure measurement - Pressure effects - Thin films - Rocket thrust - Specific impulse - Electric propulsion - Ion currents - Ions - Rocket engines - Thrust
Edition Identifiers:
- The Open Library ID: OL15504881M - OL15368969M - OL18121410M - OL17572106M - OL17125871M
- Online Computer Library Center (OCLC) ID: 39946913
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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2Advanced low-cost O₂/H₂ engines for the SSTO application
By B. David Goracke
“Advanced low-cost O₂/H₂ engines for the SSTO application” Metadata:
- Title: ➤ Advanced low-cost O₂/H₂ engines for the SSTO application
- Author: B. David Goracke
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - [National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - Washington, D.C
“Advanced low-cost O₂/H₂ engines for the SSTO application” Subjects and Themes:
- Subjects: ➤ Closed cycles - Liquid propellant rocket engines - Engine design - Single stage to orbit vehicles - Specific impulse - Thermodynamic cycles - Propulsion system configurations
Edition Identifiers:
- The Open Library ID: OL17135169M - OL17595871M - OL15501899M - OL18120519M
- Online Computer Library Center (OCLC) ID: 42711061
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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3Benefits of low-power electrothermal propulsion
By Steven R. Oleson
“Benefits of low-power electrothermal propulsion” Metadata:
- Title: ➤ Benefits of low-power electrothermal propulsion
- Author: Steven R. Oleson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Benefits of low-power electrothermal propulsion” Subjects and Themes:
- Subjects: ➤ Low earth orbits - Small satellite technology - Resistojet engines - Specific impulse - Stationkeeping - Propulsion system configurations
Edition Identifiers:
- The Open Library ID: OL17125129M - OL17565449M - OL18118438M - OL15497577M
- Online Computer Library Center (OCLC) ID: 39725552
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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4A low-erosion starting technique for high-performance arcjets
By John M. Sankovic
“A low-erosion starting technique for high-performance arcjets” Metadata:
- Title: ➤ A low-erosion starting technique for high-performance arcjets
- Author: John M. Sankovic
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - Washington, DC
“A low-erosion starting technique for high-performance arcjets” Subjects and Themes:
- Subjects: ➤ Mass flow rate - Electric ignition - Pressure pulses - Specific impulse - Electric propulsion - Starting - Arc jet engines
Edition Identifiers:
- The Open Library ID: OL17113849M - OL17000910M - OL18075824M - OL15402636M
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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5Performance of a low-power subsonic-arc-attachment arcjet thruster
By John M. Sankovic
“Performance of a low-power subsonic-arc-attachment arcjet thruster” Metadata:
- Title: ➤ Performance of a low-power subsonic-arc-attachment arcjet thruster
- Author: John M. Sankovic
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - NASA
- Publish Date: 1993
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Performance of a low-power subsonic-arc-attachment arcjet thruster” Subjects and Themes:
- Subjects: ➤ Flow velocity - Fuel injection - Propulsion system performance - Aerodynamic stability - Specific impulse - Electric propulsion - Rocket engine design - Arc jet engines
Edition Identifiers:
- The Open Library ID: OL17117082M - OL18085535M - OL15420784M - OL17794628M
- Online Computer Library Center (OCLC) ID: 34778391
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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6Metallized 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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7Experimental 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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8Design, 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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9An analytic approximation to very high specific impulse and specific power interplanetary space mission analysis
By Craig Hamilton Williams
“An analytic approximation to very high specific impulse and specific power interplanetary space mission analysis” Metadata:
- Title: ➤ An analytic approximation to very high specific impulse and specific power interplanetary space mission analysis
- Author: Craig Hamilton Williams
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“An analytic approximation to very high specific impulse and specific power interplanetary space mission analysis” Subjects and Themes:
- Subjects: ➤ Interplanetary flight - Specific impulse - Trajectory optimization - Trajectory analysis - Interplanetary trajectories - High thrust - Space missions - High impulse - Flight time
Edition Identifiers:
- The Open Library ID: OL17796149M - OL15421605M
- Online Computer Library Center (OCLC) ID: 36360073
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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10Mission advantages of constant power, variable ISP electrostatic thrusters
By Steven R. Oleson
“Mission advantages of constant power, variable ISP electrostatic thrusters” Metadata:
- Title: ➤ Mission advantages of constant power, variable ISP electrostatic thrusters
- Author: Steven R. Oleson
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2000
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, VA
“Mission advantages of constant power, variable ISP electrostatic thrusters” Subjects and Themes:
- Subjects: Electrostatic propulsion - Propulsion system performance - Specific impulse - Trajectory planning
Edition Identifiers:
- The Open Library ID: OL17601366M - OL17717458M
- Online Computer Library Center (OCLC) ID: 47969295
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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11Characteristics of ions emitted fron high-current hollow cathodes
By Ikuya Kameyama
“Characteristics of ions emitted fron high-current hollow cathodes” Metadata:
- Title: ➤ Characteristics of ions emitted fron high-current hollow cathodes
- Author: Ikuya Kameyama
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Characteristics of ions emitted fron high-current hollow cathodes” Subjects and Themes:
- Subjects: ➤ Electric propulsion - High current - Hollow cathodes - Ion engines - Ions - Plasmas (Physics) - Propulsion system performance - Spacecraft propulsion - Specific impulse - Thrustors - Xenon
Edition Identifiers:
- The Open Library ID: OL14667633M - OL17682549M
- Online Computer Library Center (OCLC) ID: 31955556
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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12Performance of a FAKEL K10K resistojet
By Robert S. Jankovsky
“Performance of a FAKEL K10K resistojet” Metadata:
- Title: ➤ Performance of a FAKEL K10K resistojet
- Author: Robert S. Jankovsky
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Performance of a FAKEL K10K resistojet” Subjects and Themes:
- Subjects: ➤ Performance tests - Nitrogen - Xenon - Specific impulse - Propulsion system performance - Resistojet engines
Edition Identifiers:
- The Open Library ID: OL15539857M - OL17838307M
- Online Computer Library Center (OCLC) ID: 40759009
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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13The diagnostics of the external plasma for the plasma rocket
By Gerald R. Karr
“The diagnostics of the external plasma for the plasma rocket” Metadata:
- Title: ➤ The diagnostics of the external plasma for the plasma rocket
- Author: Gerald R. Karr
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“The diagnostics of the external plasma for the plasma rocket” Subjects and Themes:
- Subjects: ➤ Variable thrust - Plasma propulsion - Electric potential - Tokamak devices - Specific impulse - High temperature - Thermal plasmas - Rocket thrust - Magnetic fields - Plasmas (Physics)
Edition Identifiers:
- The Open Library ID: OL17593726M - OL15508962M
- Online Computer Library Center (OCLC) ID: 40920986
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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14Trajectory optimization of an interstellar mission using solar electric propulsion
By Craig A. Kluever
“Trajectory optimization of an interstellar mission using solar electric propulsion” Metadata:
- Title: ➤ Trajectory optimization of an interstellar mission using solar electric propulsion
- Author: Craig A. Kluever
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Trajectory optimization of an interstellar mission using solar electric propulsion” Subjects and Themes:
- Subjects: ➤ Ion engines - Systems engineering - Solar electric propulsion - Trajectory optimization - Design analysis - Mission planning - Heliosphere - Specific impulse
Edition Identifiers:
- The Open Library ID: OL15508992M
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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15Performance and endurance tests of a multipropellant resistojet for space station auxiliary propulsion
By W. Earl Morren
“Performance and endurance tests of a multipropellant resistojet for space station auxiliary propulsion” Metadata:
- Title: ➤ Performance and endurance tests of a multipropellant resistojet for space station auxiliary propulsion
- Author: W. Earl Morren
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1986
- Publish Location: [Cleveland, Ohio
“Performance and endurance tests of a multipropellant resistojet for space station auxiliary propulsion” Subjects and Themes:
- Subjects: ➤ Space stations - Electric power supplies - Electric propulsion systems - Rocket propellants - Resistojet engines - Specific impulse - Space vehicles
Edition Identifiers:
- The Open Library ID: OL16151196M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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16Design of a power management and distribution system for a thermionic-diode powered spacecraft
By Greg L. Kimnach
“Design of a power management and distribution system for a thermionic-diode powered spacecraft” Metadata:
- Title: ➤ Design of a power management and distribution system for a thermionic-diode powered spacecraft
- Author: Greg L. Kimnach
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Design of a power management and distribution system for a thermionic-diode powered spacecraft” Subjects and Themes:
- Subjects: ➤ Geosynchronous orbits - Specific impulse - Thermionic diodes - Energy conversion - Management systems - Low earth orbits - Power conditioning - High impulse - Solar thermal propulsion
Edition Identifiers:
- The Open Library ID: OL15497419M
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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17Operating characteristics of the Russian D-55 thruster with anode layer
By John M. Sankovic
“Operating characteristics of the Russian D-55 thruster with anode layer” Metadata:
- Title: ➤ Operating characteristics of the Russian D-55 thruster with anode layer
- Author: John M. Sankovic
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Operating characteristics of the Russian D-55 thruster with anode layer” Subjects and Themes:
- Subjects: ➤ . - Electromagnets - Thrust measurement - Propulsive efficiency - Specific impulse - Electric propulsion - Propulsion system performance - Rocket engines
Edition Identifiers:
- The Open Library ID: OL15401820M
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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18Scaling of ion thrusters to low power
By Michael J. Patterson
“Scaling of ion thrusters to low power” Metadata:
- Title: ➤ Scaling of ion thrusters to low power
- Author: Michael J. Patterson
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1998
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, VA
“Scaling of ion thrusters to low power” Subjects and Themes:
- Subjects: Ion engines - Specific impulse - Electric propulsion - High impulse
Edition Identifiers:
- The Open Library ID: OL15541768M
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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