D. Krejci

发表

Preliminary Assessment of Performance and Cost of a Cubesat Component of the Earth Science Decadal Survey

Daniel Selva, David Krejci, Daniel Selva, 2013 .

Design and Characterization of a Scalable ion Electrospray Propulsion System

P. Lozano, D. Krejci, C. Fucetola, 2015 .

Impact of Catalyst Length and Preheating on Transient Catalytic H2O2 Decomposition Performance

D. Krejci, R. Koopmans, C. Scharlemann, 2015 .

Performance Assessment of 1 N Bipropellant Thruster Using Green Propellants H2O2/Kerosene

D. Krejci, C. Scharlemann, K. Ponweiser, 2013 .

Modeling of Jet A1-H2O2 Autoignition in a Microrocket Combustion Chamber

F. Winter, D. Krejci, C. Scharlemann, 2013 .

Assessment of Catalysts for Hydrogen-Peroxide-Based Thrusters in a Flow Reactor

Y. Batonneau, C. Kappenstein, D. Krejci, 2013 .

Full Performance Mapping of the IFM Nano Thruster, Including Direct Thrust Measurements

Bryan D. Little, D. Krejci, B. Seifert, 2019 .

IFM Nano Thruster Electric Space Propulsion: From First Cubesat Demonstration to the First 100 Thrusters Produced

D. Krejci, A. Reissner, D. Weihrauch, 2019 .

Micro-machined ionic liquid electrospray thrusters for Cubesat applications IEPC-2017-224

P. Lozano, D. Krejci, 2017 .

I‐2d

Flavia Tata Nardini, Michele Coletti, David Krejci, 2020, Nanosatellites.

CubeSat constellation management using Ionic Liquid Electrospray Propulsion

P. Lozano, D. Krejci, Marco Gomez Jenkins, 2018, Acta Astronautica.

A survey and assessment of the capabilities of Cubesats for Earth observation

David Krejci, Daniel Selva, Daniel Selva, 2012 .

Structural impact of honeycomb catalysts on hydrogen peroxide decomposition for micro propulsion

David Krejci, Carsten Scharlemann, Karl Ponweiser, 2012 .

Space Propulsion Technology for Small Spacecraft

David Krejci, Paulo Lozano, P. Lozano, 2018, Proceedings of the IEEE.

The measurement of small flow

Jan Krejci, David Krejčí, Lucie Ježová, 2017 .

Pulsed plasma thruster performance for miniaturised electrode configurations and low energy operation

C. Scharlemann, David Krejci, S. J. Pottinger, 2011 .

Staging of electric propulsion systems: Enabling an interplanetary Cubesat

David Krejci, Paulo Lozano, Marco Gomez Jenkins, 2019, Acta Astronautica.

Porous Materials for Ion-Electrospray Spacecraft Microengines

David Krejci, Paulo Lozano, P. Lozano, 2017 .

Spatial uniformity of the current emitted by an array of passively fed electrospray porous emitters

David Krejci, Paulo Lozano, P. Lozano, 2016 .

Emission Characteristics of Passively Fed Electrospray Microthrusters with Propellant Reservoirs

David Krejci, Paulo Lozano, Robert Thomas, 2017 .

The IFM Micro FEEP thruster: a modular design for smallsat propulsion

D. Krejci, B. Seifert, 2019 .

Direct thrust and plume divergence measurements of the IFM Nano Thruster

D. Krejci, B. Seifert, A. Reissner, 2018, Advances in Space Research.

A Novel Satellite Mission Concept for Upper Air Water Vapour, Aerosol and Cloud Observations Using Integrated Path Differential Absorption LiDAR Limb Sounding

Patrick Romano, Josep Aulinas, Katharina Kern, 2012, Remote. Sens..

Propulsion for Nanosatellites

Martin Tajmar, David Krejci, Carsten Scharlemann, 2011 .

A Novel Satellite Mission Concept for Upper Air Water Vapour, Aerosol and Cloud Observations Using Integrated Path Differential Absorption LiDAR Limb Sounding

T. Krings, J. Aulinas, S. Kox, 2012, Remote. Sens..

Large number system integration aspects: on orbit data and lessons learnt from launching 144 FEEP propulsion systems

D. Krejci, A. Reissner, 2022, Journal of Electric Propulsion.