Explore: Low Thrust
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Books Results
Source: The Open Library
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Search results from The Open Library
1Multi-axis thrust measurements of the EO-1 pulsed plasma thruster
By Lynn A. Arrington
“Multi-axis thrust measurements of the EO-1 pulsed plasma thruster” Metadata:
- Title: ➤ Multi-axis thrust measurements of the EO-1 pulsed plasma thruster
- Author: Lynn A. Arrington
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: ➤ [Springfield, Va - [Cleveland, Ohio]
“Multi-axis thrust measurements of the EO-1 pulsed plasma thruster” Subjects and Themes:
- Subjects: ➤ Plasma engines - Low thrust - Rocket thrust - Propulsion system performance - Low thrust propulsion - Pulsed jet engines
Edition Identifiers:
- The Open Library ID: OL17592114M - OL15559322M - OL18138500M
- Online Computer Library Center (OCLC) ID: 43271635
Access and General Info:
- First Year Published: 1999
- 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.
Online Borrowing:
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2Low thrust rocket text facility
By Lynn A. Arrington
“Low thrust rocket text facility” Metadata:
- Title: ➤ Low thrust rocket text facility
- Author: Lynn A. Arrington
- Language: English
- Number of Pages: Median: 20
- Publisher: ➤ For sale by the National Technical Information Service - NASA
- Publish Date: 1990
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Low thrust rocket text facility” Subjects and Themes:
- Subjects: ➤ Testing - Rockets (Aeronautics) - Low thrust - Chemical propulsion - Nondestructive tests - Reaction kinetics - Thrust - Rocket test facilities
Edition Identifiers:
- The Open Library ID: OL17634494M - OL16125162M
- Online Computer Library Center (OCLC) ID: 25002802
Access and General Info:
- First Year Published: 1990
- 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.
Online Borrowing:
Online Marketplaces
Find Low thrust rocket text facility at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Thrust bearing
load. Thrust bearings come in several varieties. Thrust ball bearings, composed of bearing balls supported in a ring, can be used in low-thrust applications
Orbital maneuver
low altitude), to generate a high impulse the engine necessarily needs to achieve high thrust (impulse is by definition the time multiplied by thrust)
Hohmann transfer orbit
are also often used for these situations, but low-energy transfers which take into account the thrust limitations of real engines, and take advantage
Delta-v budget
orbit.[citation needed] Current electric ion thrusters produce a very low thrust (milli-newtons, yielding a small fraction of a g), so the Oberth effect
Turbofan
produces thrust through a combination of these two portions working together. Engines that use more jet thrust relative to fan thrust are known as low-bypass
Thrust
Thrust is a reaction force described quantitatively by Newton's third law. When a system expels or accelerates mass in one direction, the accelerated mass
Low thrust relative orbital transfer
In orbital mechanics, low-thrust relative transfer is an orbital maneuver in which a chaser spacecraft covers a specific relative distance relative to
Ion thruster
of the low thrust is low acceleration because the mass of the electric power unit directly correlates with the amount of power. This low thrust makes ion
Rocket engine
A rocket engine is a reaction engine, producing thrust in accordance with Newton's third law by ejecting reaction mass rearward, usually a high-speed jet
Spacecraft electric propulsion
time. Nuclear-electric or plasma engines, operating for long periods at low thrust and powered by fission reactors, have the potential to reach speeds much