Micro Newton Thruster Development [electronic resource] : Direct Thrust Measurements and Thruster Downscaling / by Franz Georg Hey.

Por: Hey, Franz Georg [author.]Colaborador(es): SpringerLink (Online service)Tipo de material: TextoTextoEditor: Wiesbaden : Springer Fachmedien Wiesbaden : Imprint: Springer Vieweg, 2018Edición: 1st ed. 2018Descripción: XVII, 171 p. 91 illus., 20 illus. in color. online resourceTipo de contenido: text Tipo de medio: computer Tipo de portador: online resourceISBN: 9783658212094Tema(s): Aerospace engineering | Astronautics | Aerospace Technology and AstronauticsFormatos físicos adicionales: Printed edition:: Sin título; Printed edition:: Sin título; Printed edition:: Sin títuloClasificación CDD: 629.1 Clasificación LoC:TL787-4050.22TC1-1800Recursos en línea: Libro electrónicoTexto
Contenidos:
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.
En: Springer Nature eBookResumen: 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.
Star ratings
    Valoración media: 0.0 (0 votos)
Existencias
Tipo de ítem Biblioteca actual Colección Signatura Copia número Estado Fecha de vencimiento Código de barras
Libro Electrónico Biblioteca Electrónica
Colección de Libros Electrónicos 1 No para préstamo

Acceso multiusuario

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.

UABC ; Temporal ; 01/01/2021-12/31/2023.

Con tecnología Koha