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Barry Zandbergen
Barry Zandbergen
Unknown affiliation
Verified email at tudelft.nl
Title
Cited by
Cited by
Year
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
2192013
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
58*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
522007
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
382017
Cost estimation of commercial small launch vehicles
N Drenthe, B Zandbergen, R Curran, M van Pelt
Acta Astronautica 155, 160-169, 2019
332019
Cost Estimating of Commercial Smallsat Launch Vehicles
NT Drenthe, BTC Zandbergen, MO Van Pelt
EUCASS 2017, Milan, Italy, 2017
332017
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
282011
Thermal Rocket Propulsion
BTC Zandbergen
TU Delft Faculty of Aerospace Engineering, 2001
262001
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
252015
Thermal rocket propulsion
B Zandbergen
TU-Delft, Aerospace engineering, 2003
242003
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
222007
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
212006
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
192019
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
182008
Pressurization system for a cryogenic propellant tank in a pressure-fed high-altitude rocket
R Hermsen, BTC Zandbergen
Eucass, Milan, Italy, 2017
172017
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
172012
DEVELOPMENT OF A SOLAR THERMAL THRUSTER SYSTEM
HCM Leenders, BTC Zandbergen
International Astronautical Congress, 2008
172008
Bare electrodynamic tape tether experiment onboard the Delfi-1 University Satellite
AM Wijnans, BTC Zandbergen, M Kruijff, EJ Van Der Heide
4th International Spacecraft Propulsion Conference 555, 2004
152004
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
142015
Implementation of the T3μPS in the Delfi-n3Xt Satellite
C Müller, LP Lebbink, B Zandbergen, G Brouwer, R Amini, D Kajon, ...
Small Satellite Missions for Earth Observation: New Developments and Trends …, 2010
13*2010
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Articles 1–20