Deployable Structures in the CubeSat Program MOVE
作者： U. Walter , M. Langer , C. Olthoff , N. Maghaldadze , H. Baier
DOI:
关键词: Mechanism (engineering) 、 Aerospace engineering 、 Smart memory 、 Antenna (radio) 、 Simulation 、 Shell (computing) 、 Solar power 、 Satellite 、 Engineering 、 Software deployment 、 CubeSat
摘要: This paper investigates the utilization of deployable and expandable structures for communication purposes solar power generation on CubeSats. We present design on-orbit results flight-proven solar-panel release mechanism first satellite Technische Universitat Munchen First-MOVE, as well preliminary a panel deployment based smart memory alloys second MOVE II. Preliminary studies CFRS (carbon fibre reinforced silicone) shell membrane antenna two other possible payloads II are briefly described.
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