A novel design of a deployable CubeSat for material exposure missions in low earth orbit
Author:
Funder
National Natural Science Foundation of China
Publisher
Springer Science and Business Media LLC
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://link.springer.com/content/pdf/10.1007/s12567-022-00470-z.pdf
Reference43 articles.
1. Gilmore D. G.: Spacecraft Thermal Control Handbook, volume 1: Fundamental Technologies. El Segundo, CA (2002). https://doi.org/10.2514/4.989117
2. Blockley, R., Shyy, W.: Encyclopedia of aerospace engineering. American Institute of Aeronautics and Astronautics, Inc (2010). https://doi.org/10.1002/9780470686652
3. Miller, S.K., Banks, B.A., Waters, D.L.: Investigation into the differences between atomic oxygen erosion yields of materials in ground-based facilities and LEO. High Perform. Polym. 20(4–5), 523–534 (2008). https://doi.org/10.1177/0954008308089711
4. Engelhart, D.P., Cooper, R., Cowardin, H., Maxwell, J., Plis, E., Ferguson, D., Hoffmann, R.: Space weathering experiments on spacecraft materials. J. Astronaut. Sci. 66(2), 210–223 (2019). https://doi.org/10.1007/s40295-019-00175-2
5. Leger, L.: Oxygen atom reaction with shuttle materials at orbital altitudes-Data and experiment status. In 21st Aerospace Sciences Meeting (1983). https://doi.org/10.2514/6.1983-73
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