Bistable Deployable Composite Booms with Parabolic Cross Sections

IF 1.3 4区 工程技术 Q2 ENGINEERING, AEROSPACE Journal of Spacecraft and Rockets Pub Date : 2023-11-30 DOI:10.2514/1.a35840
Andrew J. Lee, Juan M. Fernandez, Jacob G. Daye
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Abstract

The stable extended and coiled states of thin-shelled composite booms with parabolic cross sections are investigated in this paper. These conic shapes potentially offer greater stiffness properties when compared to circular cross sections, which is critical for improving the load-bearing performance of deployed booms. Inducing bistability through composite layups in parabolic booms would allow for controllable self-deployment due to a less energetic coiled state when compared to monostable booms. An inextensional analytical model is used to predict the stable coiled diameters of tape spring and collapsible tubular mast (CTM) booms with parabolic cross sections. The parabolic section is discretized into circular segments using biarc spline interpolation, which allows them to be integrated into the strain energy minimization procedure used to obtain the equilibrium states. When the parabolic booms are parametrically compared against circular booms with identical layups, flattened height, and mass, the former are found to generally have better stiffness performance while being less efficient in stowed volume, as evidenced by larger coiled diameters. Analytical coiled diameters and their strain energy are verified with finite element simulations for an optimal parabolic tape spring and CTM booms. Additional validation of the parabolic tape spring’s coiled diameter is provided by experimental measurements of boom specimens.
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具有抛物线截面的双稳态可部署复合材料围油栏
本文研究了具有抛物线截面的薄壳复合材料围油栏的稳定伸展和盘绕状态。与圆形截面相比,这些圆锥形截面可能具有更大的刚度特性,这对于提高布放围油栏的承载性能至关重要。与单稳态围油栏相比,抛物线型围油栏通过复合材料层叠诱导双稳态,可实现能量较低的盘绕状态,从而实现可控的自布放。本文采用非伸展分析模型来预测带状弹簧和具有抛物线截面的可折叠管状桅杆 (CTM) 围油栏的稳定盘绕直径。使用双曲线样条插值将抛物线截面离散为圆形段,这样就可以将它们整合到用于获得平衡状态的应变能最小化程序中。将抛物面围油栏与具有相同铺层、扁平高度和质量的圆形围油栏进行参数比较后发现,前者一般具有更好的刚度性能,但收纳体积效率较低,卷绕直径较大就是证明。通过对最佳抛物面胶带弹簧和 CTM 吊杆进行有限元模拟,验证了分析得出的盘绕直径及其应变能。通过对吊杆试样的实验测量,对抛物线形胶带弹簧的卷曲直径进行了进一步验证。
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来源期刊
Journal of Spacecraft and Rockets
Journal of Spacecraft and Rockets 工程技术-工程:宇航
CiteScore
3.60
自引率
18.80%
发文量
185
审稿时长
4.5 months
期刊介绍: This Journal, that started it all back in 1963, is devoted to the advancement of the science and technology of astronautics and aeronautics through the dissemination of original archival research papers disclosing new theoretical developments and/or experimental result. The topics include aeroacoustics, aerodynamics, combustion, fundamentals of propulsion, fluid mechanics and reacting flows, fundamental aspects of the aerospace environment, hydrodynamics, lasers and associated phenomena, plasmas, research instrumentation and facilities, structural mechanics and materials, optimization, and thermomechanics and thermochemistry. Papers also are sought which review in an intensive manner the results of recent research developments on any of the topics listed above.
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