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Micro Newton Thruster Entwicklung: Direktschubmessungen und Thruster Downs-
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eBay-Artikelnr.:395159197605
Artikelmerkmale
- Artikelzustand
- ISBN-13
- 9783658212087
- Type
- NA
- Publication Name
- NA
- ISBN
- 9783658212087
- Book Title
- Micro Newton Thruster Development : Direct Thrust Measurements and Thruster Downscaling
- Publisher
- Springer Fachmedien Wiesbaden Gmbh
- Item Length
- 8.3 in
- Publication Year
- 2018
- Format
- Hardcover
- Language
- English
- Illustrator
- Yes
- Genre
- Technology & Engineering
- Topic
- Engineering (General), Aeronautics & Astronautics
- Item Weight
- 125 Oz
- Item Width
- 5.8 in
- Number of Pages
- Xvii, 171 Pages
Über dieses Produkt
Product Identifiers
Publisher
Springer Fachmedien Wiesbaden Gmbh
ISBN-10
365821208X
ISBN-13
9783658212087
eBay Product ID (ePID)
22038600314
Product Key Features
Book Title
Micro Newton Thruster Development : Direct Thrust Measurements and Thruster Downscaling
Number of Pages
Xvii, 171 Pages
Language
English
Topic
Engineering (General), Aeronautics & Astronautics
Publication Year
2018
Illustrator
Yes
Genre
Technology & Engineering
Format
Hardcover
Dimensions
Item Weight
125 Oz
Item Length
8.3 in
Item Width
5.8 in
Additional Product Features
Number of Volumes
1 vol.
Table Of Content
Electric Propulsion Fundamentals: Thrust Measurement Fundamentals, HEMPT Physics.- Micro-Newton Thruster Test Facility Development.- Micro-Newton Thrust Balance Development.- High Efficiency Multistage Plasma Thruster Downscaling.
Synopsis
Franz Georg Hey summarises the development and testing of a micro-Newton thrust balance, as well as the downscaling of a High Efficiency Multistage Plasma Thruster to micro-Newton thrust levels. The balance is tailored to fully characterise thruster candidates for the space based gravitational wave detector LISA. Thus, thrust noise measurements in sub-micro-Newton regime can be performed in the overall LISA bandwidth. The downscaled thruster can be operated down to serval tens of micro-Newton with a comparably high specific impulse. About the Author Franz Georg Hey works as mechanical, thermal, propulsion architect and technical lead of the micro-Newton propulsion laboratory of Europe's leading air and spacecraft manufacturer. The author is participating on major programmes for future satellite and electric propulsion development. The author's research is performed in close collaboration with the Dresden University of Technology, the University of Bremen and the DLR Bremen., Electric Propulsion Fundamentals: Thrust Measurement Fundamentals, HEMPT Physics.- Micro-Newton Thruster Test Facility Development.- Micro-Newton Thrust Balance Development.- High Efficiency Multistage Plasma Thruster Downscaling., Franz Georg Hey summarises the development and testing of a micro-Newton thrust balance, as well as the downscaling of a High Efficiency Multistage Plasma Thruster to micro-Newton thrust levels. The balance is tailored to fully characterise thruster candidates for the space based gravitational wave detector LISA. Thus, thrust noise measurements in sub-micro-Newton regime can be performed in the overall LISA bandwidth. The downscaled thruster can be operated down to serval tens of micro-Newton with a comparably high specific impulse. About the Author Franz Georg Hey works as mechanical, thermal, propulsion architect and technical lead of the microNewton propulsion laboratory of Europe's leading air and spacecraft manufacturer. The author is participating on major programmes for future satellite and electric propulsion development. The author's research is performed in close collaboration with the Dresden University of Technology, the University of Bremen and the DLR Bremen.
LC Classification Number
TL1-4050
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