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Survivability assessment of spacecraft impacted by orbit debris
Authors:Di-qi Hu  Bao-jun Pang  Run-qiang Chi  Zhang-chi Song  Hao Wu
Affiliation:Hypervelocity Impact Research Center,Harbin Institute of Technology,150080,Harbin,China;Hypervelocity Impact Research Center,Harbin Institute of Technology,150080,Harbin,China;Beijing Institute of Aerospace Automatic Control,100854,Beijing,China;Hypervelocity Impact Research Center,Harbin Institute of Technology,150080,Harbin,China;Changchun Institute of Optics,Fine Mechanics and Physics,Chinese Academy of Sciences,130033,Changchun,China
Abstract:To help optimize the spacecraft design and reduce the risk of spacecraft mission failure, a new approach to assess the survivability of spacecraft in orbit is presented here, including the following three steps:1) Sensitivity Analysis of spacecraft. A new sensitivity analysis method, a ray method based on virtual outer wall, is presented here. Using rays to simulate the debris cloud can effectively address the component shadowing issues. 2) Component Vulnerability analysis of spacecraft. A function"Component functional reduction degree — Component physical damage degree"is provided here to clearly describe the component functional reduction. 3) System-level Survivability Assessment of spacecraft. A new method based on expert knowledge reasoning, instead of traditional artificial failure tree method, is presented here to greatly improve the efficiency and accuracy of calculation.
Keywords:Survivability  Hypervelocity impact  Orbit debris  Ray method
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