Zobrazeno 1 - 7
of 7
pro vyhledávání: '"BISIN, Riccardo"'
Autor:
Bisin, Riccardo, Paravan, Christian
Publikováno v:
In Acta Astronautica May 2023 206:284-298
Publikováno v:
In Acta Astronautica November 2020 176:494-509
Autor:
Carlotti, Stefania, Maggi, Filippo, Ferreri, Alessandro, Galfetti, Luciano, Bisin, Riccardo, Saile, Dominik, Gülhan, Ali, Groll, Christopher, Langener, Tobias
Publikováno v:
In Acta Astronautica May 2019 158:361-374
Low regression rate is nowadays the main issue of hybrid rocket engines (HREs). The exploitation of paraffin-based fuels could be the answer to this problem. In the present study, ballistic behavior of HTPB and paraffin-based fuel blends are studied
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ce16079bb94bd54644905ccbb2ccbfef
http://hdl.handle.net/11311/1104774
http://hdl.handle.net/11311/1104774
Autor:
BENETTI, Michele, BENETTI, Mose, BISIN, Riccardo, SHIMIZU, Tomohiro, PARAVAN, Christian, MAGGI, Filippo
Deorbiting missions by means of a solid rocket motor represent a viable solution to implement mitigation actions against the proliferation of new debris population. This specific technology is flight-proven, simple to implement, and fits the main per
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d541bca3c0078ca369a2594150fe6296
Autor:
Carlotti, Stefania, Ferreri, Alessandro, Bisin, Riccardo, Maggi, Filippo, Galfetti, Luciano, Saile, Dominik, Gülhan, Ali, Langener, Tobias
An intrusive technique for the collection of the condensed combustion products in the proximity of the rocket nozzle is proposed. In particular, a supersonic probe able to withstand the harsh environment of a plume was sized to handle a progressive d
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::242c69f094e12d746246914cffb02a74
https://elib.dlr.de/126716/
https://elib.dlr.de/126716/
Autor:
MAGGI, Filippo, BISIN, Riccardo, FERRERI, Alessandro, CARLOTTI, Stefania, GALFETTI, Luciano, GROLL, Christopher, LANGENER, Tobias
The EMAP (Experimental Modelling of Alumina Particulate in Solid Booster) activity is a project funded under ESA\'s Basic Technology Research Program (TRP) for the characterization of the plume exhausted from a metalized solid rocket motor and measur
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5ef7df562ff7e114f36675a678c2c179