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 | 30 | 2012 |
Numerical prediction of aerothermodynamic effects on a re-entry vehicle body flap configuration M Di Clemente, M Marini, S Di Benedetto, A Schettino, G Ranuzzi Acta Astronautica 65 (1-2), 221-239, 2009 | 25 | 2009 |
Aerodynamic and aerothermodynamic data base of Expert capsule A Schettino, R Votta, P Roncioni, M Di Clemente, M Gerritsma, C Chiarelli, ... Proceedings of the west-east high speed flow field conference, 19-22, 2007 | 19 | 2007 |
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 | 16 | 2012 |
Hypersonic test analysis by means of aerothermal coupling methodology and infrared thermography M Di Clemente, G Rufolo, A Ianiro, G Cardone AIAA journal 51 (7), 1755-1769, 2013 | 15 | 2013 |
Shock Wave Boundary Layer Interaction in EXPERT Flight Conditions and" Scirocco" PWT M Di Clemente, M Marini, A Schettino AIAA/CIRA 13th International Space Planes and Hypersonics Systems and …, 2005 | 12 | 2005 |
CFD modelling and simulations of the HYPROB regenerative LOX/CH4 thrust chamber P Roncioni, D Cardillo, M Panelli, D Ricci, M Di Clemente, F Battista 5th European Conference For Aeronautics And Space Sciences (EUCASS), 2013 | 11 | 2013 |
Test design methodologies for flight relevant plasma wind tunnel experiments M Marini, S Di Benedetto, G Rufolo, M Di Clemente, S Borrelli Invited Lecture at West-East High Speed Flow Field WEHSFF-2007 Conference …, 2007 | 11 | 2007 |
Evaluation of local effects of transitional Knudsen number on shock wave boundary layer interactions R Votta, G Ranuzzi, A Schettino, M Marini 39th AIAA Thermophysics Conference, 4545, 2007 | 9 | 2007 |
Aerothermal Environment Definition for a Reusable Experimental Reentry Vehicle Wing Leading Edge F Battista, GC Rufolo, M Di Clemente 46th AIAA Thermophysics Conference Miami AIAA 4048, 2007 | 7 | 2007 |
Plasma Wind Tunnel Test Design Methodologies for Re-entry Vehicle Components S Di Benedetto, M Di Clemente, M Marini 2nd European Conference for Aerospace Sciences (EUCASS), 2007 | 7 | 2007 |
Aerothermal Enviroment Definition for a Reusable Experimental Re-Entry Vehicle Wing F Battista, G Rufolo, M Di Clemente 39th AIAA Thermophysics Conference, 4048, 2007 | 7 | 2007 |
Numerical investigation of RCS jet interaction and plume impingement for Mars precision landing R Votta, E Trifoni, G Pezzella, M Di Clemente, A Schettino, V Mareschi, ... 8th AIAA Theoretical Fluid Mechanics Conference, 3350, 2017 | 6 | 2017 |
Hybrid rocket technology in the frame of the italian HYPROB program M Di Clemente, R Votta, G Ranuzzi, F Ferrigno ESA 8th European Symposium on ATD for Space Vehicles, 2015 | 6 | 2015 |
Injection system design of an N2O-paraffin hybrid rocket demonstrator G Elia, M Invigorito, M Di Clemente, R Votta, G Ranuzzi Young International Conference, Aachen, Germany, 2015 | 5 | 2015 |
Numerical prediction of nozzle ablation in hybrid rocket engine M Panelli, D Cardillo, M Di Clemente, G Ranuzzi 6th EUCASS 29, 2015 | 5 | 2015 |
An extrapolation from flight methodology for a re-entry vehicle wing leading edge test in a plasma wind tunnel facility M Di Clemente, G Rufolo, F Battista 39th AIAA Thermophysics Conference, 3895, 2007 | 5 | 2007 |
Shock Wave Boundary Layer Interactions in SCIROCCO Plasma Wind Tunnel M Di Clemente, M Marini, A Schettino East West High Speed Flow Field Conference, Beijing, China, 19-22, 2005 | 5 | 2005 |
Aeroshape trade-off and aerodynamic analysis of the space-rider vehicle M Marini, M Di Clemente, G Guidotti, G Rufolo, O Lambert, N Joiner, ... 7th European Conference for Aeronautics and Space Sciences (EUCASS), 20, 2017 | 4 | 2017 |
A new global approach to evaluate the surface catalytic efficiency of tps materials based on arc jet experiments and numerical predictions E Trifoni, S Di Benedetto, M Di Clemente 8th European Symposium on Aerothermodynamics for Space Vehicles, 2015 | 4 | 2015 |