This is a list of publications on which DARE has contributed over the years. The Engineering Challenges posed by developing rocket systems provides a good ground to contribute to -and learn form the scientific community. Over the years we have published many papers on several different international conferences such as the International Astronautical Congress and the Joint Propulsion Conference last year in the US.
Very little of this work would have been possible without the support from the staff of the Space Systems Engineering Department at the TU Delft. We would specifically like to thank Ir. B.T.C. Zandbergen and Dr. A. Cervone.
T. Knop et al. (2015). Failure Mode Investigation of a Sorbital-based Hybrid Rocket FLight Motor for the Stratos II Sounding Rocket. 51st AIAA/SAE/ASEE Joint Propulsion Conference.
J. Wink et al. (2014). Test Campaign on a 10 kN Class Sorbitol-Based Hybrid Rocket Motor for the Stratos II Sounding Rocket. Space Propulsion Conference 2014.
A. Cervone and A. Fraters (2014). Combustion Instabilities and Spontaneous Engine Operation Shifting in a High Mass Flux N2O-PMMA Hybrid Rocket Engine. ESA Space Propulsion 2014 Conference.
T. Knop et al. (2013). Sorbitol-Based Hybrid Fuel Studies with Nitrous Oxide for the Stratos II Sounding Rocket. 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
A. Fraters et al. (2011). Development of a Hybrid Rocket Engine for the Stratos II Rocket. International Astronautical Congress.
S. Engelen, H. Olthof and L. Souverein (2008). Evaluating the Satine-T1 Hybrid Rocket Engine. International Astronautical Congress 2008.
S. Engelen, H. Olthof, L. Souverein and M. UItendaal (2007). Development of the Satine-T1 Hybrid Rocket Engine. International Astronautical Congress 2007.
H. Olthof, O. Motsyk and E. Jansen (2010). Development of a Solid Rocket Propellant To Accomplish the Goal of Reaching Space by a Student-Built Rocket. International Astronautical Congress 2010.
R. Hermsen and B. Zandbergen (2017). Pressurization system for a cryogenic propellant tank in a pressure-fed high-altitude rocket. EUCASS 2017.
R. Hermsen et al. (2016). Cryogenic Rocket Engine Development at Delft Aerospace Rocket Engineering. ESA Space Propulsion 2016 Conference.
A. Cervone, B. Buyens, J. Heldens and E. Slachter (2014). Experimental Investigation of the Combustion Characteristics of an Ethane-Nitrous Oxide Bi-Propellant Rocket Engine. ESA Space Propulsion 2014 Conference.
S. Engelen, P. Batenburg and L. Souverein (2008). The Deimos III Engine Concept. International Astronautical Congress 2008.
M. Mostert, B. Zandbergen and S. Engelen (2008). Preliminary Design and Development of a Moderate Thrust Liquid Oxygen/Methane Rocket Thruster. 5th International Spacecraft Propulsion Conference 2008.
S. Engelen, L. Souverein and D. Twigt (2005). Deimos Methane/Oxygen Rocket Engine Test Results. International Astronautical Congress 2005.
L. Souverein, D. Twigt and S. Engelen (2004). Amateur Gas-Propelled Rocket Engine Development and Advanced Rocket Design. International Astronautical Congress 2004.
L. Pepermans, M. Rozemeijer, E. Menting, N. Suard and S. Khurana (2018). Systematic Design of a Parachute Recovery System for the Stratos III Student Built Sounding Rocket. 2018 Atmospheric Flight Mechanics Conference.