Laser & Optoelectronics Progress, Volume. 55, Issue 3, 030002(2018)
Review on Splicing Structure Technology of Large Aperture Space Primary Mirror
Fig. 1. (a) 8 m non-splicing large aperture camera; (b) ATLAST-9.2 m; (c) ATLAST-16.8 m
Fig. 2. SMT
Fig. 3. JWST
Fig. 4. SMT stored in Naval Postgraduate School of USA
Fig. 5. Back composition introduction of JWST PM unit mirror
Fig. 6. Detail map of the ROC actuator of JWST
Fig. 7. Assembly of optical componentsand backplane of JWST
Fig. 8. ALMOST program based on SPHERES on-orbit assembly
Fig. 9. OPTIIX program based on ISS on-orbit assembly
Fig. 10. ALMOST project assembly process in ISS. SPHERES aircraft plays the role of (a) base; (b) dock; (c) monitor
Fig. 11. SPHERES for ground tests
Fig. 12. Schematic of UDP composition
Fig. 13. OPTIIX telescope and its modules
Fig. 14. Fabricated PM structure component and areal density fabricated by AHM technology
Fig. 15. Construction OPTIIX PM module
Fig. 16. MAST using modular SM groups for PM on-orbit assembly
Fig. 17. Schematic of distributed space optical telescope formation flight
Fig. 18. Flow chart of PM module installation of RAMST project
Fig. 19. General assembly flow chart of the deployable splicing optical system
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Xupeng Li, Jinfeng Shi, Wei Wang, Yongjie Wang, Xuewu Fan. Review on Splicing Structure Technology of Large Aperture Space Primary Mirror[J]. Laser & Optoelectronics Progress, 2018, 55(3): 030002
Category: General
Received: Jul. 31, 2017
Accepted: --
Published Online: Sep. 10, 2018
The Author Email: Fan Xuewu (fanxuewu@opt.ac.cn)