| A survey and assessment of the capabilities of Cubesats for Earth observation D Selva, D Krejci Acta Astronautica 74, 50-68, 2012 | 542 | 2012 |
| Emission characteristics of passively fed electrospray microthrusters with propellant reservoirs D Krejci, F Mier-Hicks, R Thomas, T Haag, P Lozano Journal of Spacecraft and Rockets 54 (2), 447-458, 2017 | 177 | 2017 |
| Space propulsion technology for small spacecraft D Krejci, P Lozano Proceedings of the IEEE 106 (3), 362-378, 2018 | 175 | 2018 |
| Design and Characterization of a Scalable ion Electrospray Propulsion System D Krejci, F Mier-Hicks, C Fucetola, P Lozano, AH Schouten, F Martel | 100 | 2015 |
| Spatial uniformity of the current emitted by an array of passively fed electrospray porous emitters C Guerra-Garcia, D Krejci, P Lozano Journal of Physics D: Applied Physics 49 (11), 115503, 2016 | 69 | 2016 |
| Endurance testing of a pulsed plasma thruster for nanosatellites D Krejci, B Seifert, C Scharlemann Acta Astronautica 91, 187-193, 2013 | 49 | 2013 |
| Demonstration of the ifm nano feep thruster in low earth orbit D Krejci, A Reissner, B Seifert, D Jelem, T Hörbe, F Plesescu, P Friedhoff, ... 4S Symposium, Sorrento, Italy, 2018 | 43 | 2018 |
| Structural impact of honeycomb catalysts on hydrogen peroxide decomposition for micro propulsion D Krejci, A Woschnak, C Scharlemann, K Ponweiser Chemical Engineering Research and Design 90 (12), 2302-2315, 2012 | 42 | 2012 |
| Development of a green bipropellant hydrogen peroxide thruster for attitude control on satellites A Woschnak, D Krejci, M Schiebl, C Scharlemann Progress in Propulsion Physics 4, 689-706, 2013 | 41 | 2013 |
| CubeSat constellation management using ionic liquid electrospray propulsion MG Jenkins, D Krejci, P Lozano Acta Astronautica 151, 243-252, 2018 | 37 | 2018 |
| Pulsed plasma thruster performance for miniaturised electrode configurations and low energy operation SJ Pottinger, D Krejci, CA Scharlemann Acta Astronautica 68 (11-12), 1996-2004, 2011 | 32 | 2011 |
| Staging of electric propulsion systems: Enabling an interplanetary Cubesat D Krejci, MG Jenkins, P Lozano Acta Astronautica 160, 175-182, 2019 | 29 | 2019 |
| Full performance mapping of the IFM Nano Thruster, including direct thrust measurements D Krejci, V Hugonnaud, T Schönherr, B Little, A Reissner, B Seifert, ... Journal of small satellites 8 (2), 881-893, 2019 | 29 | 2019 |
| Propulsion for nanosatellites C Scharlemann, M Tajmar, I Vasiljevich, N Buldrini, D Krejci, B Seifert The 32nd International Electric Propulsion Conference, Wiesbaden, Germany, 2011 | 29 | 2011 |
| Micro-machined ionic liquid electrospray thrusters for Cubesat applications D Krejci, P Lozano Proceedings of the 35th International Electric Propulsion Conference, 1-14, 2017 | 26 | 2017 |
| Recent flight data from IFM Nano Thrusters in a low earth orbit D Krejci, A Reissner, T Schönherr, B Seifert, Z Saleem, R Alejos 36th International Electric Propulsion Conference, 15-20, 2019 | 25 | 2019 |
| Development, production, and testing of the IFM nano FEEP thruster T Schönherr, B Little, D Krejci, A Reissner, B Seifert 36th International Electric Propulsion Conference, 1-11, 2019 | 24 | 2019 |
| Porous materials for ion-electrospray spacecraft microengines J Rojas-Herrera, I Jivanescu, D Freeman, D Krejci, C Fucetola, P Lozano Journal of Nanomechanics and Micromechanics 7 (3), 04017006, 2017 | 20 | 2017 |
| Hydrogen peroxide decomposition for micro propulsion: simulation and experimental verification D Krejci, A Woschnak, C Scharlemann, K Ponweiser 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 5855, 2011 | 20 | 2011 |
| Scalable ionic liquid electrospray thrusters for nanosatellites D Krejci, P Lozano Proceedings of the 39th Annual AAS GNC Conference. Breckenridge: American …, 2016 | 19 | 2016 |
Paulo LozanoAeronautics and Astronautics, MITVerified email at mit.edu
