Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Stefania Carlotti"'
Publikováno v:
Aerospace, Vol 11, Iss 4, p 309 (2024)
The object of this work is to study the ignition performances of promising catalytically promoted amino-based green fuels to be used in combination with rocket-grade hydrogen peroxide. The main hypergolic parameter, the ignition delay time, was exper
Externí odkaz:
https://doaj.org/article/7fddfa100d4c4e9299de2edd20c52860
Autor:
Stefania Carlotti, Filippo Maggi
Publikováno v:
Aerospace, Vol 9, Iss 10, p 561 (2022)
Conventional storable bipropellants make use of hydrazine and its derivatives as fuels and nitrogen tetroxide as an oxidizer. In recent years, the toxicity character of these chemicals pushed the propulsion community towards “green” alternatives.
Externí odkaz:
https://doaj.org/article/de2f82b8933e4605b3b3cc08b95cf22e
Autor:
Filippo Maggi, Stefania Carlotti, Luca Nichelini, Arianna Masini, Marco Adorno, Andrea Galavotti, Alberto Verga, Stefano Dossi, Agostino Neri
Publikováno v:
AIAA SCITECH 2023 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f50d8a6e46b6431e757f5e2b6b04e55e
https://doi.org/10.2514/6.2023-1515
https://doi.org/10.2514/6.2023-1515
Experimental techniques for characterization of particles in plumes of sub-scale solid rocket motors
Autor:
Filippo Maggi, Stefania Carlotti
Publikováno v:
Acta Astronautica. 186:496-507
An innovative collection methodology based on a recently developed supersonic probe enabled the collection of alumina particulate from the exhaust plume of a sub-scale solid propellant rocket motor and the comparison with quench collection bomb analy
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::859911da917b5612c0eba0f0588503bb
https://doi.org/10.1016/j.actaastro.2021.06.011
https://doi.org/10.1016/j.actaastro.2021.06.011
Autor:
Filippo Maggi, Stefania Carlotti, Christopher Groll, Alessandro Ferreri, Riccardo Bisin, Dominik Saile, Tobias Langener, Luciano Galfetti, Ali Gülhan
Publikováno v:
Acta Astronautica. 158:361-374
An intrusive technique for particles capturing in supersonic-high temperature flows to be used in solid rocket motors plume characterization is proposed. A supersonic probe for the collection of the condensed combustion products in the proximity of t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::abc121fe011955ca9afa3ee7eca43b0b
https://doi.org/10.1016/j.actaastro.2018.06.030
https://doi.org/10.1016/j.actaastro.2018.06.030
Autor:
Stefania Carlotti, Niklas Wingborg, Mattias Liljedahl, Tobias Langener, Filippo Maggi, Jeroen Van den Eynde, Dominik Saile, Ali Guelhan
Metals in solid propellants are used to improve specific impulse and increment the energy density. Their combustion generates condensed products that move along the motor chamber and are expelled through the nozzle. The discharge of liquid or solid p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2b8c5a3881519c21cfb83d44422079a4
https://elib.dlr.de/136747/
https://elib.dlr.de/136747/
Autor:
Riccardo Bisin, Christian Paravan, Giambattista Daminelli, Stefano Dossi, Giulio Riva, Filippo Maggi, Stefania Carlotti, Valerio Gaioni, Giovanni Colombo, Luciano Galfetti
Publikováno v:
AIAA Propulsion and Energy 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::73056a4a6987f4bc7f30549cff56b95d
https://doi.org/10.2514/6.2019-4271
https://doi.org/10.2514/6.2019-4271
Publikováno v:
2018 Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8e7f5a1af607283c27b2d0ec59c9b12f
https://doi.org/10.2514/6.2018-4663.c1
https://doi.org/10.2514/6.2018-4663.c1
Publikováno v:
2018 Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ee4147549a1d138d794d92c6ab23e332
https://doi.org/10.2514/6.2018-4663
https://doi.org/10.2514/6.2018-4663
Autor:
Christopher Groll, Tobias Langener, Luciano Galfetti, A. Guhlan, Dominik Saile, Stefania Carlotti, Stefano Dossi, Riccardo Bisin, Filippo Maggi
The present work aims at giving a comprehensive overview of the current development status of an intrusive probe, capable of collecting the condensed combustion products present in the exhaust of a solid rocket motors. The innovative technique was co
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::272c744dea23caf6cb8fb4b44f6bd225
https://elib.dlr.de/126487/
https://elib.dlr.de/126487/