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- W2316360037 abstract "CubeSats have tremendous potential to facilitate low-cost astrophysics and orbital science experimentation, but are limited by the proximity of sensors to interference from the satellite itself. In order to facilitate reliable data collection from sensitive instruments, deployable booms provide a means of separation from the spacecraft. In this work, a deployable carbon fiber boom was designed and tested to show feasibility at this small scale. Prototype booms with a lenticular cross section were developed in conjunction with a computational model. Mechanical testing has shown the ability to reliably flatten the booms in a bi-stable configuration so that it can be stored on a reel." @default.
- W2316360037 created "2016-06-24" @default.
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- W2316360037 date "2015-01-02" @default.
- W2316360037 modified "2023-10-04" @default.
- W2316360037 title "Design and Testing of Deployable Carbon Fiber Booms for CubeSat Non-Gossamer Applications" @default.
- W2316360037 cites W2021651982 @default.
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- W2316360037 doi "https://doi.org/10.2514/6.2015-0206" @default.
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