| Formation flying within a constellation of nano-satellites: The QB50 mission E Gill, P Sundaramoorthy, J Bouwmeester, B Zandbergen, R Reinhard Acta Astronautica 82 (1), 110-117, 2013 | 220 | 2013 |
| An example of active learning in Aerospace Engineering V Brügemann, EH Brummelen, JA Melkert, A Kamp, BA Reith, ... Research and practice of active learning in Engineering Education, 156-164, 2005 | 59* | 2005 |
| Development of a generic inflatable de-orbit device for CubeSats D Maessen, E van Breukelen, B Zandbergen, O Bergsma Proceedings of the 58th International Astronautical Congress, India, 2007 | 52 | 2007 |
| Green Micro-Resistojet Research at Delft University of Technology: New Options for Cubesat Propulsion A Cervone, B Zandbergen, D Guerrieri, M de Athayde Costa e Silva, ... CEAS Space Journal 9 (1), 111-125, 2017 | 40 | 2017 |
| Cost estimation of commercial small launch vehicles N Drenthe, B Zandbergen, R Curran, M van Pelt Acta Astronautica 155, 160-169, 2019 | 33 | 2019 |
| Cost Estimating of Commercial Smallsat Launch Vehicles NT Drenthe, BTC Zandbergen, MO Van Pelt EUCASS 2017, Milan, Italy, 2017 | 33 | 2017 |
| MEMS silicon-based resistojet micro-thruster for attitude control of nano-satellites M Mihailovic, TV Mathew, JF Creemer, BTC Zandbergen, PM Sarro 2011 16th International Solid-State Sensors, Actuators and Microsystems …, 2011 | 28 | 2011 |
| Thermal Rocket Propulsion BTC Zandbergen TU Delft Faculty of Aerospace Engineering, 2001 | 26 | 2001 |
| Conceptual design of a low-pressure micro-resistojet based on a sublimating solid propellant A Cervone, A Mancas, B Zandbergen Acta Astronautica 108, 30-39, 2015 | 25 | 2015 |
| Thermal rocket propulsion B Zandbergen TU-Delft, Aerospace engineering, 2003 | 24 | 2003 |
| Simulation of the attitude behaviour and available power profile of the DELFI-C3 spacecraft with application of the OPSIM platform F te Hennepe, BTC Zandbergen, R Hamann 1st CEAS European Air and Space Conference, Berlin, Germany, 10-13, 2007 | 23 | 2007 |
| In-orbit micro-propulsion demonstrator for PICO-satellite applications V Pallichadath, L Turmaine, A Melaika, S Gelmi, MV Ramisa, ... Acta Astronautica 165, 414-423, 2019 | 22 | 2019 |
| Development of a rocket engine igniter using the catalytic decomposition of hydrogen peroxide WA Jonker, AEHJ Mayer, BTC Zandbergen Green Propellant for Space Propulsion, 2006 | 21 | 2006 |
| Development of micro propulsion system technologies for minisatellites in the Netherlands J Moerel, HM Sanders, MC Louwerse, HV Jansen, J Boscher, ... Proceedings of Space Propulsion, 5-9, 2008 | 18 | 2008 |
| DEVELOPMENT OF A SOLAR THERMAL THRUSTER SYSTEM HCM Leenders, BTC Zandbergen International Astronautical Congress, 2008 | 18 | 2008 |
| Pressurization system for a cryogenic propellant tank in a pressure-fed high-altitude rocket R Hermsen, BTC Zandbergen Eucass, Milan, Italy, 2017 | 17 | 2017 |
| Application of an Advanced Micro-Propulsion System to the DelFFi Formation-Flying Demonstration Within the QB50 Mission A Cervone, B Zandbergen, J Guo, E Gill, WC Schuurbiers IAF 63rd International Astronautical Congress, 2012 | 17 | 2012 |
| Bare electrodynamic tape tether experiment onboard the DELFI-1 University Satellite AM Wijnans, BTC Zandbergen, M Kruijff, EJ Van Der Heide Proceedings of the 4th International Spacecraft Propulsion Conference (ESA …, 2004 | 15 | 2004 |
| Simple mass and size estimation relationships of pump fed rocket engines for launch vehicle conceptual design B Zandbergen 6TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS), 15, 2015 | 14 | 2015 |
| Correlating thermal balance test results with a thermal mathematical model using evolutionary algorithms N van Zijl, B Zandbergen, B Benthem Faculty of Aerospace Engineering, Delft University of Tecnology, 2013 | 13 | 2013 |
Angelo CervoneDelft University of TechnologyVerified email at tudelft.nl
