Paper
24 November 2021 Design of deployment systems for high-resolution deployable telescope based on CubeSat
Haobin Dai, Chuang Li, Liangliang Li, Bin Hu, Pei Yao
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Abstract
In this paper, the deployment systems of a deployable space telescope for CubeSat are proposed. This telescope can achieve a ground resolution less than 1 meter at an orbital altitude of 400 km. Both the primary and secondary mirrors of it can be stowed in 3U volume(100mm×100mm×300mm)during launching period. The functions of the deployment systems include the locking of the primary and secondary mirrors when stowed, the deployment on-orbit, and the active adjustment of the primary mirror segments after deployment. In this paper, firstly, the optical system of deployable telescope is described, then the deployment systems of the telescope are designed. Finally, the modal analysis is carried out using finite element method.
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Haobin Dai, Chuang Li, Liangliang Li, Bin Hu, and Pei Yao "Design of deployment systems for high-resolution deployable telescope based on CubeSat", Proc. SPIE 12069, AOPC 2021: Novel Technologies and Instruments for Astronomical Multi-Band Observations, 1206918 (24 November 2021); https://doi.org/10.1117/12.2606896
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KEYWORDS
Mirrors

Telescopes

Optical instrument design

Space telescopes

Finite element methods

Image resolution

Mirror structures

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