Thermal Stability Design of Asymmetric Support Structure for an Off-Axis Space Camera

With the development of space optical remote sensing technology, especially off-axis space cameras, the thermal dimensional stability of the support structure has become increasingly demanding. However, the asymmetry of the camera structure has not been fully considered in the past design of the thermal stability of off-axis cameras. In order to solve this problem, a support structure with very low thermal deformation in the asymmetric direction is presented in this paper for an off-axis TMA camera. By means of the negative axial thermal expansion coefficient of carbon-fiber-reinforced plastics (CFRP), a composite laminate with near zero-expansion was obtained by adjusting the direction of fiber laying, and the asymmetric feature of the off-axis remote sensing camera structure was fully considered, thus enabling the support structure to have good thermal dimensional stability. We carried out a thermal load analysis and an optical analysis of the whole camera in the case of a temperature rise of 5 °C. The results show that the zero-expansion support structure has good thermal stability, and the thermal deformation in the asymmetric direction of the camera is obviously smaller than that of the isotropic laminate support structure. Compared with the isotropic support structure, the influence of thermal deformation on MTF is reduced from 10.43% to 2.61%. This study innovatively incorporates the asymmetry of the structure into the thermal sta-bility design of an off-axis TMA camera and provides a reference for the thermal stability design of other off-axis space cameras.

[1]  S. Dhakate,et al.  Significance of Carbon Fiber Orientation on Thermomechanical Properties of Carbon Fiber Reinforced Epoxy Composite , 2021, Fibers and Polymers.

[2]  Jinxin Wang,et al.  Improvement of a computer-aided alignment algorithm for the nonsymmetric off-axis reflective telescope. , 2021, Applied optics.

[3]  Donglin Ma,et al.  Design of a high-throughput telescope based on scanning an off-axis three-mirror anastigmat system. , 2021, Applied optics.

[4]  T. Goto,et al.  Development of CFRP with Polyaniline-based Resin using Curable Dopants Employing Storage Stable Prepregs , 2021, Applied Composite Materials.

[5]  M. Ferraris,et al.  Adhesive Joining of Zerodur–CFRP–Zerodur Sandwich Structures for Aerospace Applications , 2020 .

[6]  Bin Fan,et al.  Simplified unobscured optics design for a diffractive telescope. , 2020, Applied optics.

[7]  Nan Wu,et al.  Deformation behavior of high accuracy carbon fiber-reinforced plastics sandwiched panels at low temperature , 2019, Journal of Astronomical Telescopes, Instruments, and Systems.

[8]  Yonggang Wang,et al.  Design and manufacture of 1.3 meter large caliber light-weighted Space optical components , 2019, International Conference on Space Optics.

[9]  Hirohisa Hara,et al.  Design of all-reflective space-borne 1-m aperture solar optical telescope , 2019, International Conference on Space Optics.

[10]  Lei Wei,et al.  Thermal compensation design of truss structure for large-scale off-axis three-mirror space telescope , 2019, Optical Engineering.

[11]  Yongjie Xie,et al.  Athermalization for the supporting structure of space camera primary and secondary mirrors , 2019, International Conference on Photonics and Optical Engineering and the Annual West China Photonics Conference.

[12]  Lei Yu,et al.  Thermal Design to Meet Stringent Temperature Gradient/Stability Requirements of Space Camera’s Tube , 2018, Lecture Notes in Electrical Engineering.

[13]  Giuseppina Micela,et al.  The optical configuration of the telescope for the ARIEL ESA mission , 2018, Astronomical Telescopes + Instrumentation.

[14]  Fuqiang Li,et al.  Optomechanical stability design of space optical mapping camera , 2018, International Conference on Optical Instruments and Technology.

[15]  Zhengtao Zhang,et al.  Thermal design and verification of the large-temperature-difference space optical system , 2017, 2017 IEEE International Conference on Mechatronics and Automation (ICMA).

[16]  Lei Wei,et al.  Design and optimization of the CFRP mirror components , 2017 .

[17]  Lei Wei,et al.  Design and optimization for main support structure of a large-area off-axis three-mirror space camera. , 2017, Applied optics.

[18]  A. Senba,et al.  Sensitivity analysis of thermal deformation of CFRP laminate reflector due to fiber orientation error , 2016 .

[19]  Y. Jianguo,et al.  Design and application of composite platform with extreme low thermal deformation for satellite , 2016 .

[20]  Jae-Hung Han,et al.  EFFECTS OF DIMENSIONAL STABILITY FOR SPACE TELESCOPE COMPOSITE STRUCTURES , 2015 .

[21]  Peiji Guo,et al.  Active deformation and engineering analysis of CFRP mirror of various lay-up sequences within quasi-isotropic laminates , 2014, Other Conferences.

[22]  Bo Chen,et al.  Opto-mechanisms design of extreme-ultraviolet camera onboard Chang E lunar lander. , 2014, Optics express.

[23]  A. Zenkour Hygrothermal effects on the bending of angle-ply composite plates using a sinusoidal theory , 2012 .

[24]  Yu Fan,et al.  Three Mirrors Aberrations Optical Transform Function with the Thermal Elastic Deformation , 2011 .

[25]  Virginia G. Ford,et al.  Passive thermal compensation of the optical bench of the Galaxy Evolution Explorer , 2004, SPIE Optics + Photonics.

[26]  B. Thomas,et al.  Design manufacture and testing of a composite support structure for spacecraft application , 2020 .

[27]  Chia-Ray Chen,et al.  Composite materials application on FORMOSAT-5 remote sensing instrument structure , 2017 .