David Krejci
David Krejci
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A survey and assessment of the capabilities of Cubesats for Earth observation
D Selva, D Krejci
Acta Astronautica 74, 50-68, 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
Space propulsion technology for small spacecraft
D Krejci, P Lozano
Proceedings of the IEEE 106 (3), 362-378, 2018
Design and Characterization of a Scalable ion Electrospray Propulsion System
D Krejci, F Mier-Hicks, C Fucetola, P Lozano, AH Schouten, F Martel
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
Endurance testing of a pulsed plasma thruster for nanosatellites
D Krejci, B Seifert, C Scharlemann
Acta Astronautica 91, 187-193, 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
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
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
CubeSat constellation management using ionic liquid electrospray propulsion
MG Jenkins, D Krejci, P Lozano
Acta Astronautica 151, 243-252, 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
Staging of electric propulsion systems: Enabling an interplanetary Cubesat
D Krejci, MG Jenkins, P Lozano
Acta Astronautica 160, 175-182, 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
Propulsion for nanosatellites
C Scharlemann, M Tajmar, I Vasiljevich, N Buldrini, D Krejci, B Seifert
The 32nd International Electric Propulsion Conference, Wiesbaden, Germany, 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
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
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
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
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
Scalable ionic liquid electrospray thrusters for nanosatellites
D Krejci, P Lozano
Proceedings of the 39th Annual AAS GNC Conference. Breckenridge: American …, 2016
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