Implementation of the T 3 μPS in the Delfi-n3Xt Satellite
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This chapter presents the interfaces that exist between the TNO, TU-Delft and UTwente developed micro propulsion system experiment (T3μPS) and the Delfi-n3Xt satellite currently under development at TU-Delft. Delfi-n3Xt is successor to Delfi-C3, the first Dutch student nano-satellite. Delfi-n3Xt, like its predecessor is a 3-unit cubesat, but is more advanced in that it is equipped with an active three-axis attitude determination and control system, eclipse power and a high speed data link.
[1] Vincent R. Lalli,et al. Training Manual for Elements of Interface Definition and Control , 1997 .
[2] Pascal Pempie,et al. LIQUID ROCKET ENGINE TEST PLAN COMPARISON , 2001 .
[3] J. Bouwmeester,et al. IMPROVED COMMAND AND DATA HANDLING SYSTEM FOR THE DELFI-N3XT NANOSATELLITE , 2008 .