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The Delfi-C3 mission, initiated in November 2004, is an ambitious low-cost, short time-to-delivery mission. The goal to launch the satellite by the end of 2006 results in an overall development time of two years. Adhering to such a short time frame without losing track of completeness and precision requires a Systems Engineering (SE) approach. Where applicable, the standard SE approach is reduced and adapted to the overall design philosophy of being innovative while keeping things reliable, simple and fast.  To avoid delays as a result of technology readiness issues, an important design requirement is to be independent of payloads and other new technologies flown. For convenient organization reasons, payloads are considered as separate subsystems, as can be seen in Fig. 3. This way, time tracking and control of the development of these payloads can be done at the highest level. Furthermore, to accelerate the whole design process from concept studies to verification and testing, both system and subsystems design are performed concurrently, with overlapping design phases as a result. The team, consisting of students with different but interdisciplinary backgrounds, is cooperating in a central office facing the in-house Clean Room facilities, improving communications and therewith easing design difficulties like decision making and interface control.
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