Conference Contribution | Integration and Testing of Vacuum Arc Thrusters for the pico satellite UWE-4. Kramer A, Bangert P. 66th International Astronautical Congress, Jerusalem, Israel, 2015.
UWE-3 - Lessons learned and Future Perspectives. Bangert P, Busch S, Dombrovski S, Kramer A, Schilling K. 3rd IAA conference on University SatelliteMissions, Rome, Italy, 2015.
Netsat: A four pico/nano-satellite mission for demonstration of autonomous formation flying. Schilling K, Bangert P, Busch S, Dombrovski S, Freimann A, Kleinschrodt A, Islas G, Kramer A, Nogueira T, Ris D, Scharnagl J, Tzschichholz T, Zhou L. 66th International Astronautical Congress, Jerusalem, Israel, 2015.
NanoFEEP on UWE platform - Formation Flying ofCubeSats using Miniaturized Field Emission Electric Propulsion Thrusters. Bock D, Kramer A, Bangert P, Schilling K, Tajmar M. 34th International Electric Propulsion conference, Kobe, Japan, 2015.
Design of the UWE-./ Picosatellite Orbit Control System using Vacuum-Arc-Thrusters. Kronhaus I, Schilling K, Jayakumar A, Kramer A, Pietzka M, Schein J. 33rd International Electric Propulsion Conference, Washington, D.C., USA, 2013.
Guidance Navigation and Control for Future Miniature Satellite Formations: Current Limitations and Impeding Advancements. Bangert P, Busch S, Kramer A, Schilling K. 201h IF AC Symposium on Automation and Control in Aerospace, Sherbrooke, Canada, 2016.
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