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- W3005762018 abstract "The strap-on launch vehicle is widely adopted in order to increase the launching capability of the launch vehicle, especially in the unmanned system. The connect and separation equipment between the core and the booster is one of the most key techniques in the aerospace unmanned system. In this paper, the mechanical property of the astronautic separation equipment is researched based on the different axial stiffness in tension and compression characteristics, which could be simulated as the bi-linear spring model. With the single degree of freedom analytical schematic model, every design parameter that affects the separation equipment's stiffness is researched, which can optimize the astronautic separation equipment's mechanical property. This method can provide a reference and a basis for the aerospace unmanned system design." @default.
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- W3005762018 date "2019-10-01" @default.
- W3005762018 modified "2023-09-27" @default.
- W3005762018 title "Optimization of the Separation Equipment in the Aerospace Unmanned System" @default.
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- W3005762018 doi "https://doi.org/10.1109/icus48101.2019.8996062" @default.
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