دنبال کردن
Christian Paravan
Christian Paravan
PhD, Dept. of Aerospace Science and Technology (DAER), Politecnico di Milano
ایمیل تأیید شده در polimi.it
عنوان
نقل شده توسط
نقل شده توسط
سال
Characterization of HTPB-based solid fuel formulations: Performance, mechanical properties, and pollution
LT DeLuca, L Galfetti, F Maggi, G Colombo, L Merotto, M Boiocchi, ...
Acta astronautica 92 (2), 150-162, 2013
1382013
Activated aluminum powders for space propulsion
F Maggi, S Dossi, C Paravan, LT DeLuca, M Liljedahl
Powder Technology 270, 46-52, 2015
942015
Combustion of HTPB-based solid fuels loaded with coated nanoaluminum
A Sossi, E Duranti, M Manzoni, C Paravan, LT DeLuca, AB Vorozhtsov, ...
Combustion Science and Technology 185 (1), 17-36, 2013
762013
Non-Isothermal Oxidation of Aluminum Nanopowder Coated by Hydrocarbons and Fluorohydrocarbons
A Sossi, E Duranti, C Paravan, LT DeLuca, AB Vorozhtsov, AA Gromov, ...
Applied Surface Science 271, 337-343, 2013
742013
Time-resolved burning of solid fuels for hybrid rocket propulsion
LT DeLuca, L Galfetti, G Colombo, F Maggi, A Bandera, M Boiocchi, ...
Advances in Propulsion Physics 2, 341-362, 2010
632010
A new strategy for the reinforcement of paraffin-based fuels based on cellular structures: The armored grain—Mechanical characterization
R Bisin, C Paravan, S Alberti, L Galfetti
Acta Astronautica 176, 494-509, 2020
612020
Accelerated ageing of micron-and nano-sized aluminum powders: Metal content, composition and non-isothermal oxidation reactivity
C Paravan, A Verga, F Maggi, L Galfetti
Acta Astronautica 158, 397-406, 2019
382019
Characterization and combustion of aluminum nanopowders in energetic systems
LT De Luca, L Galfetti, F Maggi, G Colombo, C Paravan, A Reina, S Dossi, ...
Metal nanopowders: production, characterization, and energetic applications …, 2014
362014
Iron oxide as solid propellant catalyst: A detailed characterization
F Maggi, S Dossi, C Paravan, L Galfetti, R Rota, S Cianfanelli, G Marra
Acta Astronautica 158, 416-424, 2019
352019
Experimental evaluation of HTPB/paraffin fuel blends for hybrid rocket applications
JC Thomas, C Paravan, JM Stahl, AJ Tykol, FA Rodriguez, L Galfetti, ...
Combustion and Flame 229, 111386, 2021
332021
Aggregation and incipient agglomeration in metallized solid propellants and solid fuels for rocket propulsion
L De Luca, C Paravan, A Reina, M Spreafico, E Marchesi, F Maggi, ...
46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 6752, 2010
322010
A critical analysis of paraffin-based fuel formulations for hybrid rocket propulsion
C Paravan, L Galfetti, F Maggi
53rd AIAA/SAE/ASEE Joint Propulsion Conference, 4830, 2017
312017
Combustion processes in hybrid rockets
C Paravan, L Galfetti, R Bisin, F Piscaglia
International Journal of Energetic Materials and Chemical Propulsion 18 (3), 2019
292019
Ballistics of innovative solid fuel formulations for hybrid rocket engines
C PARAVAN
Politecnico di Milano, 2012
282012
Nano-sized and mechanically activated composites: Perspectives for enhanced mass burning rate in aluminized solid fuels for hybrid rocket propulsion
C Paravan
Aerospace 6 (12), 127, 2019
272019
Vortex combustion in a lab-scale hybrid rocket motor
C Paravan, J Glowacki, S Carlotti, F Maggi, L Galfetti
52nd AIAA/SAE/ASEE Joint Propulsion Conference, 4562, 2016
272016
Time-resolved regression rate of innovative hybrid solid fuel formulations
C Paravan, A Reina, A Sossi, M Manzoni, G Massini, G Rambaldi, ...
Progress in Propulsion Physics 4, 75-98, 2013
272013
An optical time-resolved technique of solid fuels burning for hybrid rocket propulsion
L DeLuca, L Galfetti, F Maggi, G Colombo, C Paravan, A Reina, P Tadini, ...
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 5753, 2011
272011
Prospects of aluminum modifications as energetic fuels in chemical rocket propulsion
LT DeLuca, F Maggi, S Dossi, M Fassina, C Paravan, A Sossi
Chemical rocket propulsion: A comprehensive survey of energetic materials …, 2017
252017
Testing and Modeling Fuel Regression Rate in a Miniature Hybrid Burner
L Fanton, C Paravan, LT De Luca
International Journal of Aerospace Engineering, 15, 2012
232012
سیستم در حال حاضر قادر به انجام عملکرد نیست. بعداً دوباره امتحان کنید.
مقاله‌ها 1–20