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Daniele Pavarin
Daniele Pavarin
Professore Associato Propulsione Aerospaziale Università di Padova
Verified email at unipd.it - Homepage
Title
Cited by
Cited by
Year
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
1142013
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
872019
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
812020
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
732009
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
642013
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
572013
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
512020
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
492022
Development of a counterbalanced pendulum thrust stand for electric propulsion
F Trezzolani, M Magarotto, M Manente, D Pavarin
Measurement 122, 494-501, 2018
492018
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
482003
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
442017
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
422020
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
412014
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
412012
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
402013
Improvement of the CISAS high-shot-frequency light-gas gun
D Pavarin, A Francesconi
International journal of impact engineering 29, 549-562, 2003
372003
Parametric study of a cathode-less radio frequency thruster
M Magarotto, D Pavarin
IEEE Transactions on Plasma Science 48 (8), 2723-2735, 2020
342020
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
342011
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
342011
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
332003
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