Structural and Thermal Analysis of a CubeSat
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-99-1665-8_32
Reference11 articles.
1. Bouwmeester J, Menicucci A, Gill EKA (2002) Improving CubeSat reliability: subsystem redundancy or improved testing? Reliab Eng Syst Saf 220(Dec 2021):108288. https://doi.org/10.1016/j.ress.2021.108288
2. Villela T, Costa CA, Brandão AM, Bueno FT, Leonardi R (2019) Towards the thousandth CubeSat: a statistical overview. Int J Aerosp Eng 2019. https://doi.org/10.1155/2019/5063145
3. Rafael L, De Aguiar C, Henrique S, Ribeiro D, Paiano S. Modal analysis of a satellite with different materials
4. Kassner ME, Geantil P, Li X (2011) A study of the quench sensitivity of 6061-T6 and 6069-T6 aluminum alloys. J Metall 2011:1–5. https://doi.org/10.1155/2011/747198
5. Finckenor MM (2018) Materials for spacecraft. In: Aerospace materials and applications, pp 403–434. https://doi.org/10.2514/5.9781624104893.0403.0434
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