Volgen
Michele Ferraiuolo
Michele Ferraiuolo
Geverifieerd e-mailadres voor cira.it
Titel
Geciteerd door
Geciteerd door
Jaar
Heat transfer in a multi-layered thermal protection system under aerodynamic heating
M Ferraiuolo, O Manca
International Journal of Thermal Sciences 53, 56-70, 2012
672012
Design and development of a LOX/LCH4 technology demonstrator
V Salvatore, F Battista, R Votta, M Di Clemente, M Ferraiuolo, P Roncioni, ...
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 3935, 2012
302012
Thermo-structural design of a Ceramic Matrix Composite wing leading edge for a re-entry vehicle
M Ferraiuolo, R Scigliano, A Riccio, E Bottone, M Rennella
Composite Structures 207, 264-272, 2019
212019
Thermostructural design of a flying winglet experimental structure for the EXPERT re-entry test
M Ferraiuolo, A Riccio, M Gigliotti, D Tescione, R Gardi, G Marino
202009
Single-injector LOX/GCH4 combustion chambers manufacturing and experimental characterization in the framework of the HYPROB-BREAD project
F Battista, M Ferraiuolo, P Natale, D Cardillo, A French, D Ricci, ...
Space Propulsion Conference, 2014
162014
Development of a LOX/LCH4 Technology Demonstrator Based on Regenerative Cooling throughout Validation of Critical Design Aspects with Breadboards in the Framework of the Hyprob …
F Battista, M Di Clemente, M Ferraiuolo, R Votta, D Ricci, M Panelli, ...
63rd International Astronautical Congress, Naples, Italy. IAC-2012, 2012
162012
On the thermo-structural response of a composite closeout in a regeneratively cooled thrust chamber
M Ferraiuolo, W Petrillo, A Riccio
Aerospace Science and Technology 71, 402-411, 2017
152017
On the adoption of global/local approaches for the thermomechanical analysis and design of liquid rocket engines
M Ferraiuolo, M Leo, R Citarella
Applied Sciences 10 (21), 7664, 2020
142020
A comparative study of refined and simplified thermo-viscoplastic modeling of a thrust chamber with regenerative cooling
M Ferraiuolo, V Russo, K Vafai
International Communications in Heat and Mass Transfer 78, 155-162, 2016
142016
Modelling, Testing and Design Considerations of a GOX/GCH4 Igniter for a HYPROB-SSBB Single Injector Thrust Chamber
F Battista, M Ferraiuolo, A Martucci, M Fragiacomo, P Natale, D Ricci, ...
Journal of the British Interplanetary Society 1 (2014), 67, 2014
132014
Contact sensitivity analysis of a coupling pin for the nose cap of a launch re-entry vehicle
M Ferraiuolo, A Riccio, D Tescione, R Gardi, G Marino
57th International Astronautical Congress, C2. 1.08, 2008
132008
Thermal–Mechanical FEM Analyses of a Liquid Rocket Engines Thrust Chamber
M Ferraiuolo, M Perrella, V Giannella, R Citarella
Applied Sciences 12 (7), 3443, 2022
122022
Thermo-structural and thermo-fluid dynamics analyses supporting the design of the cooling system of a methane liquid rocket engine
M Ferraiuolo, D Ricci, F Battista, P Roncioni, V Salvatore
ASME International Mechanical Engineering Congress and Exposition 46421 …, 2014
122014
Methane transcritical behavior in the cooling system of the HYPROB-BREAD LOX/LCH4 demonstrator rocket engine
D Ricci, F Battista, M Ferraiuolo, V Salvatore, M Fragiacomo
ASME International Mechanical Engineering Congress and Exposition 57342 …, 2015
112015
The HYPROB demonstrator line: status of the LOX/LCH4 propulsion activities
F Battista, D Ricci, P Natale, D Cardillo, M Fragiacomo, M Ferraiuolo, ...
8th European Conference for Aeronautics and Space Sciences, EUCASS2019 …, 2019
102019
Development of a Liquid Rocket Ground Demonstrator through thermal analyses
D Ricci, F Battista, M Ferraiuolo, P Natale, M Fragiacomo
Heat Transfer Engineering, 2019
92019
Hyprob Project: Status of the Technological and Experimental Activities of the LRE Development Line
F Battista, D Ricci, P Natale, D Cardillo, M Fragiacomo, M Ferraiuolo, ...
Proceedings of the Space Propulsion, 2018
92018
Thermostructural numerical analysis of the thrust chamber of a liquid propellant rocket engine
R Citarella, M Ferraiuolo, M Perrella, V Giannella
Materials 15 (15), 5427, 2022
72022
Thermal analyses supporting the design of the Hyprob sub-scale calorimetric breadboard
D Ricci, M Ferraiuolo, F Battista, V Salvatore
Proc. ASMEATI-UIT 2015 Conference on Thermal Energy Systems: Production …, 2015
72015
Design of an experimental campaign on methane regenerative liquid rocket engine cooling system
R Votta, F Battista, M Ferraiuolo, P Roncioni, V Salvatore, P De Matteis
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, 4146, 2013
72013
Het systeem kan de bewerking nu niet uitvoeren. Probeer het later opnieuw.
Artikelen 1–20