Výsledky vyhledávání

Mechanically Amplified Milli-Newton Thrust Balance for Direct Thrust Measurements of Electric Thrusters for Space Propulsion

Autor: Jaume Navarro-Cavallé, P. Fajardo, Mick Wijnen

Publikováno v: e-Archivo: Repositorio Institucional de la Universidad Carlos III de Madrid
Universidad Carlos III de Madrid (UC3M)
IEEE Transactions on Instrumentation and Measurement
e-Archivo. Repositorio Institucional de la Universidad Carlos III de Madrid
instname

Direct thrust measurements by means of a thrust balance (TB) are the golden standard for measuring thrust and, concurrently, the specific impulse in electric thrusters. To measure these properties in the novel class of electrodeless plasma thrusters,

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0f37b60578f3996121928ef712ccdd4d
https://doi.org/10.1109/tim.2020.3037305

Zobrazit plný text záznamu

Helicon and ECR plasma sources for space propulsion: simulation and testing

Autor: Jaume Navarro-Cavallé, Eduardo Ahedo, Mario Merino, Alvaro Sanchez-Villar, Mick Wijnen, P. Fajardo, J Zhou

Publikováno v: 2019 International Conference on Electromagnetics in Advanced Applications (ICEAA).

This paper summarizes experimental activities on an Space Helicon Plasma Thruster (HPT) prototype and modeling developments of both the HPT and the Electron Cyclotron Resonance Thruster (ECRT). The modeling summary is centered on the propagation and

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::2f01e4380adc4d44990aaf2007da511a
https://doi.org/10.1109/iceaa.2019.8879300

Zobrazit plný text záznamu

CubeSat Lunar Positioning System Enabled by Novel On-Board Electric Propulsion

Autor: Nereida Agüera-Lopez, Mick Wijnen, Sara Correyero-Plaza, Daniel Perez-Grande

Publikováno v: e-Archivo. Repositorio Institucional de la Universidad Carlos III de Madrid
instname

Due to the advances in miniaturization, CubeSats are becoming more versatile, with projected mission capabilities that are traditionally reserved for larger satellites. However, they are still limited by a lack of efficient propulsive means. A novel

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::55205ad9fc9cfcf90d22f339701e6c28
https://hdl.handle.net/10016/33373

Zobrazit plný text záznamu

Experimental characterization of a 1 kW Helicon Plasma Thruster

Autor: Eduardo Ahedo, P. Fajardo, Jaume Navarro-Cavallé, Mick Wijnen

Publikováno v: e-Archivo. Repositorio Institucional de la Universidad Carlos III de Madrid
instname
e-Archivo: Repositorio Institucional de la Universidad Carlos III de Madrid
Universidad Carlos III de Madrid (UC3M)

A Helicon Plasma Thruster has been tested in the 500-1000 W radio-frequency power range, at 13.56 MHz. In order to determine its propulsive performances, a parametric study of some operational parameters has been carried out, including the exploratio

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3fb20d61ae422f905c9d66ac696188b3
https://doi.org/10.1016/j.vacuum.2017.11.036

Zobrazit plný text záznamu

Vyhledávací nástroje:

Upřesnit hledání