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Evaluation of the Effect of the Compression Stiffness and the Bending Stiffness on the Deployment of a Membrane-like Spacecraft with the Multi-particle Method

机译:评估压缩刚度和弯曲刚度对多颗粒法造成膜状航天器展开的影响

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In this study, we modify multi-particle method, a calculation method for predicting membrane behaviour, for evaluating collision between membranes and the change in membrane compression and bending stiffness due to devices mounted on membrane. This modification is verified its validity by the consistency with the results of the experiments conducted in the previous study. Then, we investigate the changes in the deployment behaviour when the temperature and thickness of solar cells change.
机译:在该研究中,我们改变多颗粒方法,用于预测膜行为的计算方法,用于评估膜之间的碰撞以及由于安装在膜上的装置引起的膜压缩和弯曲刚度的变化。 该修改通过与前一项研究中进行的实验结果的一致性核实其有效性。 然后,我们调查太阳能电池的温度和厚度改变时部署行为的变化。

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