Abstract
Owing to the rapid developments in space technology, there has been a substantial increase in the demand for large-diameter and low-mass space-borne deployable antennas with high geometric stability. To meet this demand, this paper presents a novel single mobility deployable ring mechanism with a high deploy/fold ratio. This mechanism is suitable for constructing large-scale satellite deployable antennas. First, a basic truss element with a low storage height is proposed, and fundamental parameters of the deployable mechanism are analyzed. Second, a general motion analysis model of the deployment process is established, and the corresponding cable-net structure is designed. Finally, a ground experimental prototype with a diameter of 5.0 m is fabricated to demonstrate the feasibility of the proposed mechanism. Based on the experimental results, the feasibility and effectiveness of the novel deployable antenna proposed herein are verified.
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