1. Finite Element Analysis of Radiation Dosimetric Model during Lift-Off
- Author
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Zhou Mingcong, Wang Ke, Fan Qing-wen, Xiong Liangying, Sun Fenghui, Dong Xiangping, Jiang Wenjun, Wang Jun-feng, and Pei Hongliang
- Subjects
RDM ,Spacecraft ,business.industry ,Computer science ,Acoustics ,Modal analysis ,Radiation ,Response spectrum ,business ,Statics ,Imaging phantom ,Space environment - Abstract
Space rays can cause serious damage to the vital organs of astronauts. To assess the radiation safety of astronauts in the space environment, the most direct and effective way is to send radiation equivalent phantoms equipped with various radiation sensors into space through the spacecraft, and collect relevant radiation data. The phantom will be subjected to a large impact load during the lift-off of spacecraft, leading the various layers of the phantom to be dislocated or crushed, which will affect the collection of radiation data. Based on the Chengdu Dosimetric Phantom (CDP) and according to the distribution and installation requirements of radiation sensors, the phantom is sliced in multiple layers and connected by a center rod to obtain a model for space radiation dose collection, called Radiation Dosimetric Model (RDM). According to the mechanical parameters of the spacecraft during lift-off, we use Ansys Workbench Software to conduct Statics, Modal and Response Spectrum analysis of the RDM. Under a static load of 6.5g, we calculate the stress and deformation of the layers and the center rod of the RDM, as well as their size and distribution, carry out modal analysis, and calculate the maximum response of the RDM under a given acceleration spectrum with a load peak value of 6.5g. The result shows that under the dynamic and static load of 6.5g, the layers and the center rod will not be dislocated, crushed, etc. This ensures the safety of Radiation Dosimetric Model during the lift-off process, and has important theoretical significance and practical value.
- Published
- 2020
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