Zobrazeno 1 - 10
of 25
pro vyhledávání: '"J Gonzalez Del Amo"'
Autor:
Alexander Reissner, David Krejci, P. Silvestrin, J. Gonzalez del Amo, Bernhard Seifert, Luca Massotti
Publikováno v:
CEAS Space Journal. 14:109-124
ESA’s Next Generation Gravity Mission (NGGM) is a candidate Mission of Opportunity for ESA-NASA cooperation in the frame of the MAss change and Geosciences International Constellation (MAGIC) . The mission aims at enabling long-term monitoring of t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8cb6a8a9cb9df3bef412853b036cf217
https://doi.org/10.1007/s12567-021-00386-0
https://doi.org/10.1007/s12567-021-00386-0
Autor:
K. Holste, Daniel Spemann, Peter J. Klar, J. Gonzalez del Amo, Kathe Dannenmayer, Horst Neumann, A. Bulit, Hans Leiter, Fabrizio Scortecci, Christoph Eichhorn, Carsten Bundesmann, Frank Scholze
Publikováno v:
Procedia Engineering. 185:1-8
Recently, we have set up an Advanced Electric Propulsion Diagnostic (AEPD) platform [1] , which allows for the in-situ measurement of a comprehensive set of thruster performance parameters. The platform utilizes a five-axis-movement system for precis
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9226064fe6b696c68a3b8c4ed0060cb2
https://doi.org/10.1016/j.proeng.2017.03.283
https://doi.org/10.1016/j.proeng.2017.03.283
Autor:
Frank Scholze, Christoph Eichhorn, Horst Neumann, J. Gonzalez del Amo, Carsten Bundesmann, Daniel Spemann, D. Feili, A. Bulit
A performance model of a radio frequency plasma bridge neutralizer was developed to calculate the electrical parameters and optimize the neutralizer design. Minimization of power losses and gas consumption, and a maximization of the neutralizer lifet
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2ca7aa07f09cb917d7661b0b9ffb619b
Autor:
N. Buldrini, F. Plesescu, W. Grienauer, J. Gonzalez del Amo, B. Carnicero-Domínguez, I. Vasiljevich, M. Betto, Martin Tajmar
Publikováno v:
Scopus-Elsevier
Future scientific satellites require precision pointing capabilities with thrust levels from sub-µN to the mN-range and very low thrust noise. Since 2004, a dedicated mN FEEP thruster based on the space-proven ARC Indium Liquid-Metal-Ion-Sources is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ec8604344f824864ebc6723661e33de2
https://doi.org/10.2514/6.2008-4534
https://doi.org/10.2514/6.2008-4534
Autor:
J. C. Bastante, B. Carnicero-Domínguez, V. Fernández, S. Cornara, J. Gonzalez del Amo, L.F. Peñín, M. Price
Publikováno v:
57th International Astronautical Congress.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b7fa08aa9f7abeb69727771ebe1cdfc4
https://doi.org/10.2514/6.iac-06-c1.6.09
https://doi.org/10.2514/6.iac-06-c1.6.09
Autor:
Orson Sutherland, R. Franzen, E. Gengembre, J. Gonzalez del Amo, C. Costa, G. Saccoccia, Roger Walker, Jeff Kingwell, Paul R. Alexander, A.J. Parfitt, Christine Charles, Pierre-Etienne Frigot, Rod Boswell, Leigh Pfitzner
Publikováno v:
42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
The Helicon Double Layer Thruster is a new type of magneto-plasma thruster which combines the helicon technology for an efficient coupling of the electrical power to the plasma and a current-free double layer (formed spontaneously in the physical and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::077dd40a3327851d7618d4fc3d16f578
https://doi.org/10.2514/6.2006-4838
https://doi.org/10.2514/6.2006-4838
Autor:
B. Carnicero-Domínguez, A. Caramagno, J. Gonzalez del Amo, F. Pirondini, S. Cornara, M. Price
Publikováno v:
56th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fdfebd94f7134080d9941673d5157361
https://doi.org/10.2514/6.iac-05-c1.7.02
https://doi.org/10.2514/6.iac-05-c1.7.02
Autor:
J. Gonzalez del Amo, M. Saverdi, B. Fallis, A. Bouchoule, N. Wallace, D. Nicolini, F. Darnon, N. Kutufa, Lorenzo Casalino, G. Saccoccia, D. Estublier, L. Jolivet, E. Chesta, L. Biagioni, Salvo Marcuccio, E. Gengembre, J. P. Boeuf, P. Dumazert, Mathieu Prioul, G. Noci, M. Berti, A. Cadiou
Publikováno v:
Scopus-Elsevier
Variable-specific-impulse electric propulsion systems can provide important advantages and cost reductions to any scale of planetary mission. The first part of this paper describes their potential benefits, with special emphasis on mission analysis a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::191f556474fedeafec5201ccef393936
http://hdl.handle.net/11568/251349
http://hdl.handle.net/11568/251349