Adhesive Technology of Space Optical Sensor Transmissive Mirror Group
YANG Yu1,*, WANG Weihua2,*, LI Liansheng1, ZHANG Yao2, CHI Baihong2, JIA Yi2
1 Beijing Institute of Control Engineering, Beijing 100190, China 2 China Aerospace Science and Technology Innovation Research Institute, Beijing 100088, China
Abstract: Space optical sensors are very important parts of the spacecraft, and their reliable operation in the extreme space environment is the guarantee for the normal conduct of space activities and missions. The core of the space optical sensor lies in the manufacture of the optical system, and the current space optical sensor most commonly adopts a small and medium-aperture transmissive optical system, which requires precise assembly of the optical components. Compared with the connection method of mechanical fasteners, the adhesive method has more potential in the manufacture of small and medium-aperture transmissive optical systems; however, the adhesive method is rarely mentioned in the manufacture of optical lens systems for aerospace. In this work, the adhesive technology of the transmissive lens group for the optical system of the space optical sensor was systematically studied, the adhesive combination of XM31 as the lower layer adhesive and DP460 as the upper layer adhesive is determined through stress simulation and surface shape analysis, and the main factors influencing the shape size after the hemming are determined by L9(34) orthogonal test and range/variance analysis, and the reliability of the technology is evaluated by the space environment ground simulation experiment including thermal vacuum, temperature cycling, mechanical environment adaptability test, and the optimal adhesive technical parameters are finally determined. This research provides strong guidance for the adhesive technology of the transmission mirror group of space optical sensors in the future.
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2025, Vol. 39 
