Deployment Properties with Gravity Compensation Devices for Boom-Membrane Integrated Wrapped Structures

机译：动臂膜集成包裹结构的重力补偿装置的展开特性

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Many de-orbiting systems using deployable membranes are developed to keep the safety space environment. We have proposed a boom-membrane integrated space structure using tri-axial tubular CFRP booms. This paper describes detailed properties of the booms with and without the gravity compensation devices and fixed and free for rotation constraint of the stowage hub through the deployment experiments. We focus on the boom tip because the point where the membrane is apph'ed by the tensile forces. In the experiments we measure the tip position and calculate the time history of deploying length and tip speed. As a result, the effects of the gravity compensation devices and rotation constraint of the stowage hub to deployment of the booms are clarified, as well as the validity of the hinge deployment model has been verified.

机译：为了保持安全空间环境，开发了许多使用可展开膜的去轨道系统。我们提出了一种使用三轴管状CFRP吊杆的吊杆-膜集成空间结构。本文通过展开实验描述了具有和不具有重力补偿装置以及固定和自由约束集装轮毂旋转的动臂的详细特性。我们将重点放在动臂末端，因为通过拉力施加膜片的位置。在实验中，我们测量尖端位置并计算展开长度和尖端速度的时间历史。结果，阐明了重力补偿装置和行李箱轮毂的旋转约束对动臂展开的影响，并且验证了铰链展开模型的有效性。

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《3rd AIAA spacecraft structures conference 2016》|2016年|540-547|共8页
会议地点 San Diego CA(US)
作者
Hiroshi Furuya; Takashi Yokomatsu; Hiraku Sakamoto; Yasutaka Satou;
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Tokyo Institute of Technology, Yokohama, 226-8502, Japan;

Tokyo Institute of Technology, Yokohama, 226-8502, Japan;

Tokyo Institute of Technology, Yokohama, 226-8502, Japan;

Tokyo Institute of Technology, Yokohama, 226-8502, Japan;

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Deployment Properties with Gravity Compensation Devices for Boom-Membrane Integrated Wrapped Structures

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