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Micro Newton thruster development = ...

Hey, Franz Georg.

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Micro Newton thruster development = direct thrust measurements and thruster downscaling /

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Micro Newton thruster development/ by Franz Georg Hey.
其他題名:	direct thrust measurements and thruster downscaling /
作者:	Hey, Franz Georg.
出版者:	Wiesbaden :Springer Fachmedien Wiesbaden : : 2018.,
面頁冊數:	xvii, 171 p. :ill. (some col.), digital ;24 cm.
內容註:	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.
Contained By:	Springer eBooks
標題:	Rocket engines - Thrust. -
電子資源:	http://dx.doi.org/10.1007/978-3-658-21209-4
ISBN:	9783658212094

Micro Newton thruster development = direct thrust measurements and thruster downscaling /
Hey, Franz Georg.

Micro Newton thruster developmentdirect thrust measurements and thruster downscaling /[electronic resource] :by Franz Georg Hey. - Wiesbaden :Springer Fachmedien Wiesbaden :2018. - xvii, 171 p. :ill. (some col.), digital ;24 cm.

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. Contents 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 Target Groups Scientists and students in the field of aerospace research Satellite and thruster integrators, electric propulsion and gravitational wave detector community 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.

ISBN: 9783658212094

Standard No.: 10.1007/978-3-658-21209-4doiSubjects--Topical Terms:

3308654
Rocket engines
--Thrust.

LC Class. No.: TL782 / .H494 2018

Dewey Class. No.: 629.134354

Micro Newton thruster development = direct thrust measurements and thruster downscaling /
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520 $a 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. Contents 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 Target Groups Scientists and students in the field of aerospace research Satellite and thruster integrators, electric propulsion and gravitational wave detector community 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.
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