Micro Newton Thruster Development: Direct Thrust Measurements and Thruster Downscaling
Autor Franz Georg Heyen Limba Engleză Paperback – 19 dec 2018
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.
Toate formatele și edițiile | Preț | Express |
---|---|---|
Paperback (1) | 360.14 lei 3-5 săpt. | |
Springer Fachmedien Wiesbaden – 19 dec 2018 | 360.14 lei 3-5 săpt. | |
Hardback (1) | 369.62 lei 6-8 săpt. | |
Springer Fachmedien Wiesbaden – 14 mar 2018 | 369.62 lei 6-8 săpt. |
Preț: 360.14 lei
Nou
Puncte Express: 540
Preț estimativ în valută:
68.94€ • 75.10$ • 57.84£
68.94€ • 75.10$ • 57.84£
Carte disponibilă
Livrare economică 27 noiembrie-11 decembrie
Preluare comenzi: 021 569.72.76
Specificații
ISBN-13: 9783658248659
ISBN-10: 3658248653
Pagini: 171
Ilustrații: XVII, 171 p. 91 illus., 20 illus. in color.
Dimensiuni: 148 x 210 mm
Greutate: 0.23 kg
Ediția:Softcover reprint of the original 1st ed. 2018
Editura: Springer Fachmedien Wiesbaden
Colecția Springer Vieweg
Locul publicării:Wiesbaden, Germany
ISBN-10: 3658248653
Pagini: 171
Ilustrații: XVII, 171 p. 91 illus., 20 illus. in color.
Dimensiuni: 148 x 210 mm
Greutate: 0.23 kg
Ediția:Softcover reprint of the original 1st ed. 2018
Editura: Springer Fachmedien Wiesbaden
Colecția Springer Vieweg
Locul publicării:Wiesbaden, Germany
Cuprins
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.
Notă biografică
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.
Textul de pe ultima copertă
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.
Caracteristici
HEMPT principle can be scaled down to micro thrust levels