Active space debris removal by a hybrid propulsion module LT DeLuca, F Bernelli, F Maggi, P Tadini, C Pardini, L Anselmo, M Grassi, ... Acta Astronautica 91, 20-33, 2013 | 114 | 2013 |
REGULUS: A propulsion platform to boost small satellite missions M Manente, F Trezzolani, M Magarotto, E Fantino, A Selmo, N Bellomo, ... Acta Astronautica 157, 241-249, 2019 | 88 | 2019 |
Comparative performance assessment of plasma reactors for the treatment of PFOA; reactor design, kinetics, mineralization and energy yield M Saleem, O Biondo, G Sretenović, G Tomei, M Magarotto, D Pavarin, ... Chemical Engineering Journal 382, 123031, 2020 | 81 | 2020 |
Design of 50 W helicon plasma thruster D Pavarin, F Ferri, M Manente, D Curreli, Y Guclu, D Melazzi, D Rondini, ... 31st International Electric Propulsion Conference 20, 2009 | 73 | 2009 |
Numerical and experimental investigation of unidirectional vortex injection in hybrid rocket engines N Bellomo, F Barato, M Faenza, M Lazzarin, A Bettella, D Pavarin Journal of Propulsion and Power 29 (5), 1097-1113, 2013 | 64 | 2013 |
A microwave interferometer for small and tenuous plasma density measurements O Tudisco, A Lucca Fabris, C Falcetta, L Accatino, R De Angelis, ... Review of Scientific Instruments 84 (3), 2013 | 58 | 2013 |
3D-VIRTUS: Equilibrium condition solver of radio-frequency magnetized plasma discharges for space applications M Magarotto, D Melazzi, D Pavarin Computer Physics Communications 247, 106953, 2020 | 51 | 2020 |
Design and In-orbit Demonstration of REGULUS, an Iodine electric propulsion system N Bellomo, M Magarotto, M Manente, F Trezzolani, R Mantellato, ... CEAS Space Journal 14 (1), 79-90, 2022 | 50 | 2022 |
Development of a counterbalanced pendulum thrust stand for electric propulsion F Trezzolani, M Magarotto, M Manente, D Pavarin Measurement 122, 494-501, 2018 | 49 | 2018 |
Impact facility based upon high frequency two-stage light-gas gun F Angrilli, D Pavarin, M De Cecco, A Francesconi Acta Astronautica 53 (3), 185-189, 2003 | 48 | 2003 |
Scaling parameters of swirling oxidizer injection in hybrid rocket motors E Paccagnella, F Barato, D Pavarin, A Karabeyoğlu Journal of Propulsion and Power 33 (6), 1378-1394, 2017 | 44 | 2017 |
Numerical model of a helicon plasma thruster M Magarotto, M Manente, F Trezzolani, D Pavarin IEEE Transactions on Plasma Science 48 (4), 835-844, 2020 | 42 | 2020 |
Investigation of effect of diaphragms on the efficiency of hybrid rockets N Bellomo, M Lazzarin, F Barato, A Bettella, D Pavarin, M Grosse Journal of Propulsion and Power 30 (1), 175-185, 2014 | 41 | 2014 |
SPIREs: A finite-difference frequency-domain electromagnetic solver for inhomogeneous magnetized plasma cylinders D Melazzi, D Curreli, M Manente, J Carlsson, D Pavarin Computer Physics Communications 183 (6), 1182-1191, 2012 | 41 | 2012 |
Computational fluid dynamics simulation of regression rate in hybrid rockets M Lazzarin, F Barato, A Bettella, D Pavarin Journal of Propulsion and Power 29 (6), 1445-1452, 2013 | 40 | 2013 |
Improvement of the CISAS high-shot-frequency light-gas gun D Pavarin, A Francesconi International journal of impact engineering 29, 549-562, 2003 | 37 | 2003 |
Parametric study of a cathode-less radio frequency thruster M Magarotto, D Pavarin IEEE Transactions on Plasma Science 48 (8), 2723-2735, 2020 | 34 | 2020 |
Testing and CFD simulation of diaphragm hybrid rocket motors A Bettella, M Lazzarin, N Bellomo, F Barato, D Pavarin, M Grosse 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 6023, 2011 | 34 | 2011 |
Cfd simulation of a hybrid rocket motor with liquid injection M Lazzarin, M Faenza, F Barato, N Bellomo, A Bettella, D Pavarin, ... 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 5537, 2011 | 34 | 2011 |
Effect of hypervelocity impact on microcellular ceramic foams from a preceramic polymer P Colombo, A Arcaro, A Francesconi, D Pavarin, D Rondini, S Debei Advanced Engineering Materials 5 (11), 802-805, 2003 | 33 | 2003 |