Proceedings Paper • Open Access
Design and verification for front mirror-body structure of on-axis three mirror anastigmatic space camera
Paper Abstract
The primary and secondary mirrors of onaxis three mirror anastigmatic (TMA) space camera are connected and supported by its front mirror-body structure, which affects both imaging performance and stability of the camera. In this paper, the carbon fiber reinforced plastics (CFRP) thin-walled cylinder and titanium alloy connecting rod have been used for the front mirror-body opto-mechanical structure of the long-focus on-axis and TMA space camera optical system. The front mirror-body component structure has then been optimized by finite element analysis (FEA) computing. Each performance of the front mirror-body structure has been tested by mechanics and vacuum experiments in order to verify the validity of such structure engineering design.
Paper Details
Date Published: 20 November 2017
PDF: 6 pages
Proc. SPIE 10564, International Conference on Space Optics — ICSO 2012, 105643L (20 November 2017); doi: 10.1117/12.2309049
Published in SPIE Proceedings Vol. 10564:
International Conference on Space Optics — ICSO 2012
Bruno Cugny; Errico Armandillo; Nikos Karafolas, Editor(s)
PDF: 6 pages
Proc. SPIE 10564, International Conference on Space Optics — ICSO 2012, 105643L (20 November 2017); doi: 10.1117/12.2309049
Show Author Affiliations
Xiaoyong Wang, Beijing Institute of Space Mechanics and Electricity (China)
Chongling Guo, Beijing Institute of Space Mechanics and Electricity (China)
Chongling Guo, Beijing Institute of Space Mechanics and Electricity (China)
Yongli Hu, Beijing Institute of Space Mechanics and Electricity (China)
Hongyan He, Beijing Institute of Space Mechanics and Electricity (China)
Hongyan He, Beijing Institute of Space Mechanics and Electricity (China)
Published in SPIE Proceedings Vol. 10564:
International Conference on Space Optics — ICSO 2012
Bruno Cugny; Errico Armandillo; Nikos Karafolas, Editor(s)
© SPIE. Terms of Use
