國立高雄大學圖資館 |

語系: 繁體中文

說明(常見問題)

圖資館首頁

登入

回首頁

切換: 標籤 | MARC模式 | ISBD

Micro Newton thruster developmentdir...

Hey, Franz Georg.

Micro Newton thruster developmentdirect 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 developmentby 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.
Contained By:	Springer eBooks
標題:	Rocket enginesThrust.
電子資源:	http://dx.doi.org/10.1007/978-3-658-21209-4
ISBN:	9783658212094$q(electronic bk.)

Micro Newton thruster developmentdirect 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$q(electronic bk.)

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

809614
Rocket engines
--Thrust.

LC Class. No.: TL782 / .H494 2018

Dewey Class. No.: 629.134354

Micro Newton thruster developmentdirect thrust measurements and thruster downscaling /
LDR:02639nmm a2200325 a 4500 001 533759
003 DE-He213
005 20180913105541.0
006 m d
007 cr nn 008maaau
008 181205s2018 gw s 0 eng d
020 $a 9783658212094$q(electronic bk.)
020 $a 9783658212087$q(paper)
024 7 $a 10.1007/978-3-658-21209-4 $2 doi
035 $a 978-3-658-21209-4
040 $a GP $c GP
041 0 $a eng
050 4 $a TL782 $b .H494 2018
072 7 $a TRP $2 bicssc
072 7 $a TTDS $2 bicssc
072 7 $a TEC002000 $2 bisacsh
082 0 4 $a 629.134354 $2 23
090 $a TL782 $b .H615 2018
100 1 $a Hey, Franz Georg. $3 809613
245 1 0 $a Micro Newton thruster development $h [electronic resource] : $b direct thrust measurements and thruster downscaling / $c by Franz Georg Hey.
260 $a Wiesbaden : $b Springer Fachmedien Wiesbaden : $b Imprint: Springer Vieweg, $c 2018.
300 $a xvii, 171 p. : $b ill. (some col.), digital ; $c 24 cm.
505 0 $a 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.
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.
650 0 $a Rocket engines $x Thrust. $3 809614
650 1 4 $a Engineering. $3 210888
650 2 4 $a Aerospace Technology and Astronautics. $3 309707
710 2 $a SpringerLink (Online service) $3 273601
773 0 $t Springer eBooks
856 4 0 $u http://dx.doi.org/10.1007/978-3-658-21209-4
950 $a Engineering (Springer-11647)