Explore: Plasma Propulsion
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Books Results
Source: The Open Library
The Open Library Search Results
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
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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2High power MPD thruster development at the NASA Glenn Research Center
By Michael R. LaPointe
“High power MPD thruster development at the NASA Glenn Research Center” Metadata:
- Title: ➤ High power MPD thruster development at the NASA Glenn Research Center
- Author: Michael R. LaPointe
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2001
- Publish Location: ➤ [Cleveland, Ohio] - Hanover, MD
“High power MPD thruster development at the NASA Glenn Research Center” Subjects and Themes:
- Subjects: Electric propulsion - Electromagnetic propulsion - Magnetoplasmadynamic thruster - Plasma propulsion - Propulsion
Edition Identifiers:
- The Open Library ID: OL16042412M - OL17621403M
- Online Computer Library Center (OCLC) ID: 55086194
Access and General Info:
- First Year Published: 2001
- 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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3The 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
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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4High voltage SPT performance
By David Manzella
“High voltage SPT performance” Metadata:
- Title: High voltage SPT performance
- Author: David Manzella
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2001
- Publish Location: ➤ Hanover, MD - [Cleveland, Ohio]
“High voltage SPT performance” Subjects and Themes:
- Subjects: Mass flow rate - Field strength - Optimization - High voltages - Plasma propulsion
Edition Identifiers:
- The Open Library ID: OL17612535M - OL16037064M
- Online Computer Library Center (OCLC) ID: 52112035
Access and General Info:
- First Year Published: 2001
- 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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5Evaluation of low power hall thruster propulsion
By David Manzella
“Evaluation of low power hall thruster propulsion” Metadata:
- Title: ➤ Evaluation of low power hall thruster propulsion
- Author: David Manzella
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Evaluation of low power hall thruster propulsion” Subjects and Themes:
- Subjects: ➤ Ion propulsion - Plasma propulsion - Plasma engines - Density measurement - Hall accelerators - Current density - Ion currents - Propulsion system performance
Edition Identifiers:
- The Open Library ID: OL17838493M
- Online Computer Library Center (OCLC) ID: 41260781
Access and General Info:
- First Year Published: 1996
- 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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6Hall thruster ion beam characterization
By David H. Manzella
“Hall thruster ion beam characterization” Metadata:
- Title: ➤ Hall thruster ion beam characterization
- Author: David H. Manzella
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Hall thruster ion beam characterization” Subjects and Themes:
- Subjects: ➤ Plasma propulsion - Rocket exhaust - Plasma engines - Ion beams - Hall accelerators - Current density - Density measurement - Ion currents
Edition Identifiers:
- The Open Library ID: OL15420746M
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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7Simplified numerical description of SPT operation
By David H. Manzella
“Simplified numerical description of SPT operation” Metadata:
- Title: ➤ Simplified numerical description of SPT operation
- Author: David H. Manzella
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Simplified numerical description of SPT operation” Subjects and Themes:
- Subjects: ➤ Gas dynamics - Plasma propulsion - Plasma jets - Ionization potentials - Ionization cross sections - Plasma engines - Plasma density - Xenon - Magnetohydrodynamic flow - Electron energy - Magnetic flux - Gas ionization
Edition Identifiers:
- The Open Library ID: OL15423161M
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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8Rapid Mars transits with exhaust-modulated plasma propulsion
By Franklin R. Chang-Diaz
“Rapid Mars transits with exhaust-modulated plasma propulsion” Metadata:
- Title: ➤ Rapid Mars transits with exhaust-modulated plasma propulsion
- Author: Franklin R. Chang-Diaz
- Number of Pages: Median: 10
- Publisher: Lyndon B. Johnson Space Center
- Publish Date: 1995
- Publish Location: Houston, Texas
“Rapid Mars transits with exhaust-modulated plasma propulsion” Subjects and Themes:
- Subjects: Plasma propulsion - Mars probes
Edition Identifiers:
- The Open Library ID: OL19004936M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Plasma propulsion engine
A plasma propulsion engine is a type of electric propulsion that generates thrust from a quasi-neutral plasma. This is in contrast with ion thruster engines
Laser propulsion
Laser propulsion is a form of beam-powered propulsion where the energy source is a remote (usually ground-based) laser system and separate from the reaction
Ion thruster
whatever their electric charge, and are specifically referred to as plasma propulsion engines, where the electric field is not in the direction of the acceleration
Nuclear pulse propulsion
Nuclear pulse propulsion or external pulsed plasma propulsion is a hypothetical method of spacecraft propulsion that uses nuclear explosions for thrust
Pulsed plasma thruster
pulsed plasma thruster (PPT), also known as a Pulsed Plasma Rocket (PPR), or as a plasma jet engine (PJE), is a form of electric spacecraft propulsion. PPTs
Spacecraft propulsion
Spacecraft propulsion is any method used to accelerate spacecraft and artificial satellites. In-space propulsion exclusively deals with propulsion systems
Variable Specific Impulse Magnetoplasma Rocket
for possible use in spacecraft propulsion. It uses radio waves to ionize and heat an inert propellant, forming a plasma, then a magnetic field to confine
MagBeam
space debris in orbit around Earth. MagBeam propulsion uses a helicon plasma source to produce a plasma beam. A helicon drive consists of a quartz tube
Magnetohydrodynamic drive
air-breathing MHD propulsion (where ambient air is ionized) that is still limited to theoretical concepts and early experiments. Plasma propulsion engines using
Magnetic sail
sail is a proposed method of spacecraft propulsion where an onboard magnetic field source interacts with a plasma wind (e.g., the solar wind) to form an