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TechnoSat

TechnoSat – Nanosatellit for the Demonstration and Verification of Novel Components and Subsystems
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The TechnoSat nanosatellite mission has the primary objective to demonstrate and test novel nanosatellite technologies and components in Low Earth Orbit. The satellite carries several payloads:

  • Camera
  • Fluiddynamic Actuator
  • S-Band Transmitter HISPICO
  • Laser-Retroreflectors
  • Solar Generator Impact Detector
  • Star Tracker STELLA
  • Rection Wheel System

The secondary mission objective of TechnoSat is the on-orbit verification of the novel adaptive nanosatellite bus TUBiX20 (TU Berlin innovative neXt generation 20 kg nanosatellite platform). TechnoSat is scheduled to be launched in 2017.

References

Frank Baumann and Klaus Brieß (2015). A Quad-channel UHF Transceiver for TUBiX20. 10th IAA Symposium on Small Satellites for Earth Observation


Merlin F. Barschke and Karsten Gordon (2015). Enabling Flexible Payload Management through Modularity. 66th International Astronautical Congress


Karsten Gordon and Merlin F. Barschke (2015). A new Concept of Software Architecture for a Flexible Attitude Determination and Control of Nanosatellites. 66th International Astronautical Congress


Karsten Gordon, Alexander Graf and Merlin F. Barschke (2015). Practical Experience in using Continuous Integration within the Development of Nanosatellite Software. 10th IAA Symposium on Small Satellites for Earth Observation, 191–194.


Danilo Költzsch and Merlin F. Barschke (2014). Development and Verification of a Lightweight and Modular Structure for a Novel Nanosatellite Platform. 63th German Aerospace Congress


Merlin F. Barschke and Karsten Gordon (2014). TUBiX20 – A Generic Systems Architecture for a Single Failure Tolerant Nanosatellite Platform. 65th International Astronautical Congress


Daniel Noack, Jonathan Ludwig and Klaus Brieß (2013). Untersuchungen zu einem fluiddynamischen Aktuator für den Einsatz auf dem Nanosatelliten TechnoSat. 62. German Aerospace Congress


Daniel Noack, Jonathan Ludwig and Klaus Brieß (2014). Fluid-Dynamic Attitude Control Experiment for TechnoSat. Small Satellites Systems and Services Symposium


Georg Kirchner, Luwig Grunwaldt, Reinhard Neubert, Franz Koidl, Merlin F. Barschke, Zizung Yoon, Hauke Fiedler and Christine Hollenstein (2013). Laser Ranging to Nano-Satellites in LEO Orbits: Plans, Issues, Simulations. presented at the 18th International Workshop on Laser Ranging


Merlin F. Barschke, Zizung Yoon and Klaus Brieß (2013). TUBiX - The TU Berlin Innovative Next Generation Nanosatellite Bus. 64th International Astronautical Congress


Merlin F. Barschke, Zizung Yoon, Stephan Roemer, and Klaus Briess (2013). Nanosatellite Acitivities at TU Berlin. 2nd IAA Conference on Universitiy Satellites Missions


Merlin F. Barschke, Karsten Großekatthöfer and Sergio Montenegro (2014). Implementation of a Nanosatellite On-Board Software based on Building-Blocks. Small Satellites Systems and Services Symposium


Merlin F. Barschke, Harry Adirim, Oleksii Balagurin, Walter Ballheimer, Lars Dornburg, Hakan Kayal, Daniel Noak, Christian Nitzschke, Nobert A. Pilz, Harald Wojtkowiak and Klaus Brieß (2013). TechnoSat - A Nanosatellite Mission for On-Orbit Technology Demonstration. 27th AIAA/USU Conference on Samll Satellites


Merlin F. Barschke, Frank Baumann, Walter Ballheimer, Karsten Großekatthöfer, Christian Nitzschke and Klaus Brieß (2013). TUBiX20 - The novel Nanosatellite Bus of TU Berlin. 9th IAA Symposium on Small Satellites for Earth Observation, 93-96.


Waldemar Bauer, Oliver Romberg, Holger Krag, Geert Henk Visser, Daniel Digirolamo, Merlin F. Barschke and Sergio Montenegro (2016). Debris in-situ impact detection by utilization of CubeSat solar panels. Small Satellites Systems and Services Symposium


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Chair of Space Technology

Prof. Dr.-Ing. Klaus Brieß
+49 30 314-21339
Room F 515

Grant No.:

50 RM 1219