Zobrazeno 1 - 10
of 49
pro vyhledávání: '"N. Buldrini"'
Publikováno v:
Advances in Space Research
The IFM Nano Thruster, which consists of a porous tungsten crown ion-emitter to provide thrust in the range of 10 µN to 1 mN at 2000–5000 s ISP, has been tested on a µN thrust balance that has previously been verified at the ESA Propulsion Labora
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9779c816e9992864afbe9d840fb8372d
Publikováno v:
53rd AIAA/SAE/ASEE Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::eee02ebc7982448cde13562a49a48b48
https://doi.org/10.2514/6.2017-4887
https://doi.org/10.2514/6.2017-4887
Autor:
R. Killinger, L. Serafini, A. Polli, M. Jentsch, L. Ceruti, D. DiCara, N. Buldrini, Carsten Scharlemann, Davide Nicolini
Publikováno v:
Acta Astronautica. 69:822-832
The Laser Interferometer Space Antenna project (LISA) is a co-operative program between ESA and NASA to detect gravitational waves by measuring distortions in the space–time fabric. LISA Pathfinder is the precursor mission to LISA designed to valid
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6f55e9aba781fcacd11d85959eda8dcb
https://doi.org/10.1016/j.actaastro.2011.05.037
https://doi.org/10.1016/j.actaastro.2011.05.037
Publikováno v:
Scopus-Elsevier
Recently, a highly integrated electric propulsion system for ultra-precise generation of thrust on spacecraft has been developed using a porous matrix through which liquid indium flows during operation. In an effort to further improve the performance
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::298856efd27bf562720cdf42be4eb0c1
https://doi.org/10.2514/6.2011-5592
https://doi.org/10.2514/6.2011-5592
Publikováno v:
Scopus-Elsevier
The Laser Interferometer Space Antenna project (LISA) is a co-operative program between ESA and NASA to detect gravitational waves by measuring distortions in the spacetime fabric. LISA Pathfinder is the precursor mission to LISA designed to validate
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::04e134414a96173b60f7ea7bc0cb61b4
https://doi.org/10.2514/6.2009-5093
https://doi.org/10.2514/6.2009-5093
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
Publikováno v:
Ultramicroscopy. 109(5)
The Austrian Research Centers have a long history of developing indium Liquid-Metal-Ion Source (LMIS) for space applications including spacecraft charging compensators, SIMS and propulsion. Specifically the application as a thruster requires long-ter
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e162ed96229daab34ec5f8ddd5141787
https://pubmed.ncbi.nlm.nih.gov/19064310
https://pubmed.ncbi.nlm.nih.gov/19064310
Publikováno v:
42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
In 1990, James F. Woodward, professor of physics at the California State University, provided a set of equations showing that it should be possible, via Mach's Principle, to change transiently the mass of a body. The major practical embodiment of the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9481acf1c32528df44b5fb8435ab10f8
https://doi.org/10.2514/6.2006-4911
https://doi.org/10.2514/6.2006-4911
Publikováno v:
42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
In the framework of the GOCE Micro-thruster Program, ARC Seibersdorf research (ARC-sr) has collected more than 18000 hours of cumulative operation with several Indium FEEP emitters. The lessons learned during this intensive test campaign allowed to g
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::aff4577abd1119555d4f5a2a9abdad2b
https://doi.org/10.2514/6.2006-4827
https://doi.org/10.2514/6.2006-4827
Autor:
Martin Tajmar, Carsten Scharlemann, Angelo Genovese, N. Buldrini, Michael Boss, Helmut Frueholz, Rainer Killinger
Publikováno v:
Scopus-Elsevier
ARC-sr together with EADS Astrium and EADS Space Transportation is jointly developing a flight design for an Indium FEEP Microthruster suitable for LISA Pathfinder. The paper reviews all basic design elements and performance parameters and shows that
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b542371a763f10f151d019e343efda85
https://doi.org/10.2514/6.2006-4826
https://doi.org/10.2514/6.2006-4826