Micro Newton Thruster Development

Lieferzeit: Lieferbar innerhalb 14 Tagen

53,49 

Direct Thrust Measurements and Thruster Downscaling

ISBN: 365821208X
ISBN 13: 9783658212087
Autor: Hey, Franz Georg
Verlag: Springer Vieweg
Umfang: xvii, 171 S., 71 s/w Illustr., 20 farbige Illustr., 171 p. 91 illus., 20 illus. in color.
Erscheinungsdatum: 14.03.2018
Auflage: 1/2018
Produktform: Gebunden/Hardback
Einband: Gebunden

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 MicroNewton Thruster Test Facility Development MicroNewton 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 AuthorFranz 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.

Artikelnummer: 3714339 Kategorie:

Beschreibung

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.

Autorenporträt

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.

Herstellerkennzeichnung:


Springer Vieweg in Springer Science + Business Media
Abraham-Lincoln-Straße 46
65189 Wiesbaden
DE

E-Mail: juergen.hartmann@springer.com

Das könnte Ihnen auch gefallen …