Main Structure of the Survey Camera for CSST: A Paradigm for Structural Design of Large-Scale Complex Space Optical Instruments

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Опубликовано в::	Aerospace vol. 12, no. 12 (2025), p. 1036-1062
Главный автор:	Jiang Renkui
Другие авторы:	Zhang, Ang, Li, Zhaoyang, Liu Enhai, Wang, Libin, Le Sixian, Zhang, Yongchao, Zhang Haini, Wang, Hongyu, Guan Shaohua, Luo Qian, Mao Yufeng, Xu, Weiqi, Chen Panke, Su Haibing, Zhang, Yanqing, Du Junfeng, Shao Junming, Huang Mingzhu, Liang, Wei
Опубликовано:	MDPI AG
Предметы:	China Load Thermal stability Structural engineering Layers Verification Spacecraft components Carbon fiber reinforced plastics Optimization Cameras Space stations Structural design Astronomical instruments Focal plane devices Structural strength Cyanates Optical instruments Carbon Composite materials Position measurement Titanium base alloys Space exploration Space telescopes Temperature Machining Sensors Resonant frequencies Design Astronauts Complexity Design optimization Vibration tests Structural stability Interfaces Contact angle
Online-ссылка:	Citation/Abstract Full Text + Graphics Full Text - PDF
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