Chinese Optics, Volume. 15, Issue 5, 1079(2022)
Flexural mounting technology of a 1.8 m space-borne rectangular mirror
Fig. 1. Schematic diagram of mounting structure of a rectangular mirror with large aperture
Fig. 2. Typical constraints for a mirror. (a) 2-2-2 Constraint; (b) 3-2-1 Constraint
Fig. 3. A bi-axial flexural hinge based on kinematic equivalence principle
Fig. 5. Schematic diagram of equivalent flexural short straight beam
Fig. 6. Relationship between
Fig. 12. Effect of
Fig. 14. Surface deformation at different
Fig. 15. Effect of different
Fig. 16. Effect of different sizes of flexural support on the RMS value
Fig. 17. Effect of different sizes of flexural supports on the first-order natural frequency
Fig. 19. Surface deformation under 1 G gravity in
Fig. 25. Schematic diagram of mirror aspheric interferometry optical testing layout
Fig. 27. The surface figure of the mirror tested in 180° direction
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Zong-xuan LI, Chang-hao ZHANG, De-fu ZHANG, Bin MA, Yun-feng LI. Flexural mounting technology of a 1.8 m space-borne rectangular mirror[J]. Chinese Optics, 2022, 15(5): 1079
Category: Original Article
Received: Jun. 13, 2022
Accepted: --
Published Online: Sep. 29, 2022
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