Zobrazeno 1 - 10
of 12
pro vyhledávání: '"Olivier Orlandi"'
Publikováno v:
Acta Astronautica. 158:470-479
This paper presents the effects of the combustion of aluminium droplets in the context of solid propulsion. A focus is made on the specific case of pressure oscillations. After a brief presentation of the characteristics of aluminium combustion, inte
Publikováno v:
Proceedings of the Combustion Institute. 33:1949-1956
The combustion in air of a 100 μm-diameter aluminum droplet is studied by direct Navier–Stokes simulations. The model only considers the gas phase and includes a reduced Al/O 2 kinetic scheme with 8 species and 10 reactions. The model is validated
Publikováno v:
International Journal of Energetic Materials and Chemical Propulsion. 8:515-530
Publikováno v:
International Journal of Energetic Materials and Chemical Propulsion. 7:99-122
Publikováno v:
International Journal of Energetic Materials and Chemical Propulsion. 6:529-550
Autor:
Olivier Orlandi, Séverine Ballereau, Jean Thepenier, Eric Robert, Franck Godfroy, Nathalie Cesco, Stany Gallier
Publikováno v:
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Large segmented Solid Rocket Motors (SRM) experience pressure oscillations. A number of them, includin g Ariane 5, Space Shuttle or the Titan family, are reported to exhibit this kind of instability during operatio n. Pressure oscillations (ODP) in s
Publikováno v:
46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
In the framework of the ORPHEE (Original Research Project on Hybrid Engine in Europe) project co-funded between the EU, industries and universities, several promising applications based on the hybrid propulsion engines offering promising advantages l
Autor:
Annamaria Russo Sorge, Carmine Carmicino, Roberto De Amicis, Marco de Rosa, Olivier Orlandi, Frederich Dauch
Publikováno v:
45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
In the framework of the Hybrid Propulsion Evaluation Program developed under the European Space Agency financial support, a series of static firing tests have been carried out on a lab-scale hybrid engine fed by gaseous oxygen and two different fuel
Autor:
Christian Perut, Iskender Gökalp, Olivier Orlandi, Guillaume Fouin, Max Calabro, Claire Franson, Christian Chauveau
Publikováno v:
Progress in Propulsion Physics
DeLuca, L.; Bonnal, C.; Haidn, O.; Frolov, S. Progress in Propulsion Physics, 2009, 978-2-7598-0411-5. ⟨10.1051/eucass/200901031⟩
DeLuca, L.; Bonnal, C.; Haidn, O.; Frolov, S. Progress in Propulsion Physics, 2009, 978-2-7598-0411-5. ⟨10.1051/eucass/200901031⟩
International audience; are a new kind chemical propel-to ensure the mechanical resistance of gram. of liquid propulsion disadvantages. is ing between motor loading and firing. It needs insulations that increase the dry mass. It is possible to limit
Autor:
P. Della Pieta, Eric Robert, Séverine Ballereau, J. Guery, Franck Godfroy, Olivier Orlandi, Stany Gallier, Nathalie Cesco
Publikováno v:
44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.