| CubeSat constellations for disaster management in remote areas G Santilli, C Vendittozzi, C Cappelletti, S Battistini, P Gessini Acta Astronautica 145, 11-17, 2018 | 86 | 2018 |
| The hollow cathode as a micro-ion thruster P Gessini, SB Gabriel, DG Fearn IEPC Paper, 01-233, 2001 | 19 | 2001 |
| Thrust characterization of a T6 hollow cathode P Gessini, SB Gabriel, DG Fearn IEPC Paper, 05-257, 2005 | 18 | 2005 |
| The T6 hollow cathode as a microthruster P Gessini, S Gabriel, D Fearn 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 4078, 2005 | 16 | 2005 |
| Hollow cathode thrust measurements using a target P Gessini, S Gabriel, D Fearn 4th International Spacecraft Propulsion Conference 555, 2004 | 14* | 2004 |
| Ablative pulsed plasma thruster system optimization for microsatellites P Gessini, G Paccani 27th International Electric Propulsion Conference, IEPC-01-182, 2001 | 13 | 2001 |
| Electric propulsion research at the University of Southampton S Pottinger, P Gessini, D Webb, R Intini Marques, SB Gabriel Journal of the British Interplanetary Society 59, 176-183, 2006 | 11 | 2006 |
| Low power ablative pulsed plasma thrusters P Gessini, LTC Habl, MND Barcelos Jr, JL Ferreira, RI Marques, M Coletti Proc. of the 33rd Int. Electric Propulsion Conf.(Washington, DC), 2013-344, 2013 | 10 | 2013 |
| A 4-gridded ion engine for high impulse mission M Coletti, P Gessini, SB Gabriel Space Propulsion, 2010 | 10 | 2010 |
| Hollow cathode thruster for all-electric spacecraft P Gessini, M Coletti, A Grubisic, S Gabriel, N Wallace, D Fearn 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 5195, 2007 | 9 | 2007 |
| A study of the thrust generated by a T6 hollow cathode P Gessini, S Gabriel, D Fearn 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 5265, 2006 | 9 | 2006 |
| Hollow cathode thrust measurement using a target: system development and calibration P Gessini, S Gabriel, D Fearn 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 4104, 2002 | 7* | 2002 |
| Solar electric propulsion for lunar transfer P Gessini, M Coletti, N Bevan, R Intini Marques, G Michalareas, S Gabriel | 6 | 2006 |
| Numerical simulation of magnetic nozzle flow for nuclear-fusion space propulsion P Turchi, P Mikellides, R Gerwin, P Gessini 35th Joint Propulsion Conference and Exhibit, 2701, 1999 | 6 | 1999 |
| Gigawatt, quasi-steady plasma flow facility for fusion rocket simulations P Turchi, P Gessini, P Mikellides, H Kamhawi, T Umeki 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 3592, 1998 | 6 | 1998 |
| A multipropellant RF plasma thruster IB Matveev, P Gessini, SI Serbin IEEE Transactions on Plasma Science 47 (1), 44-46, 2018 | 4 | 2018 |
| The thrust generated by a T6 ion engine hollow cathode P Gessini, M Coletti, SB Gabriel Acta Astronautica 102, 249-257, 2014 | 3 | 2014 |
| Preliminary performance results of a 5-cm Kaufman-type ion thruster GM Sandonato, JAN Gonçalves, RT Irita, P Gessini 32nd International Electric Propulsion Conference 1, 2011 | 2 | 2011 |
| A pendulum target balance for ion engine thrust measurement P Gessini, GM Sandonato, RT Irita, JAN Gonçalves, GF e Fernandes International Electric Propulsion Conference, 30., 2007 | 2 | 2007 |
| Enabling low-cost high-energy missions with small spacecraft by using pulsed plasma thrusters P Gessini, GC Possa, R Intini Marques, C Dobranszki, IO Golosnoy, ... | 1 | 2019 |
Rodrigo Intini MarquesResearcher, INPEVerified email at inpe.br
