Zobrazeno 1 - 10
of 24
pro vyhledávání: '"Stefano Dossi"'
Autor:
Djalal Trache, Filippo Maggi, Ilaria Palmucci, Luigi T. DeLuca, Kamel Khimeche, Marco Fassina, Stefano Dossi, Giovanni Colombo
Publikováno v:
Arabian Journal of Chemistry, Vol 12, Iss 8, Pp 3639-3651 (2019)
Oxamide (OXA) and azodicarbonamide (ADA) are among the known burning rate suppressants used in composite solid rocket propellants. Much research has been carried out to understand mechanism of suppression but literature about the action of OXA and AD
Externí odkaz:
https://doaj.org/article/01c47dc572b0407d8b8bbf9cbe914e26
Autor:
Giacomo Morselli, Marco Villa, Paola Ceroni, Luca Medici, Fabio Tarlazzi, Stefano Dossi, Pietro Matteucci, Andrea Galanti, Andrea Magrì
Publikováno v:
Polymer Engineering & Science.
Autor:
Filippo Maggi, Alessandro Finazzi, Piero Finocchi, Christian Paravan, Luciano Galfetti, Stefano Dossi, Alessandro Murgia, Tobias Lips, Geert Smet, Kobye Bodjona
Publikováno v:
AIAA SCITECH 2023 Forum.
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.
Autor:
Filippo Maggi, Alessandro Finazzi, Piero Finocchi, Christian Paravan, Luciano Galfetti, Stefano Dossi, Alessandro Murgia, Tobias Lips, Geert Smet, Kobye Bodjona
Publikováno v:
AIAA SCITECH 2023 Forum.
Publikováno v:
Polymers for Advanced Technologies. 31:864-872
Autor:
Filippo Maggi, Stefano Dossi
Publikováno v:
Propellants, Explosives, Pyrotechnics. 44:1312-1318
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.
Publikováno v:
Progress in Propulsion Physics – Volume 11.
Air-breathing solid fueled propulsion devices represent rugged, cheap, and rather simple options, out of the ramjet (RJ) category, which can contribute to volume containment and structural weight reduction. In the case of a ducted rocket, a fuel-rich
Publikováno v:
Progress in Propulsion Physics – Volume 11.
Innovative, mechanically activated Al–polytetrafluoroethylene (PTFE) composites and ammonium perchlorate (AP) coated nano-sized aluminum (C-ALEX) were produced, characterized, and tested as solid fuel additives. The ballistics of fuel formulations