Weight Optimization of Primary Mirror Used in EO Payload for Small Satellite
Author:
Publisher
Springer Singapore
Link
http://link.springer.com/content/pdf/10.1007/978-981-15-1724-2_22
Reference6 articles.
1. Yan Y, Jin G, Yang H (2007) Design and analysis of large spaceborne light-weighted primary mirror and its support system. In: 3rd International symposium on advanced optical manufacturing and testing technologies: large mirrors and telescopes, vol 6721. International Society for Optics and Photonics, p 67210V
2. Li Y (2012) Modeling and structural analysis of honeycomb structure mirror. In: Modern Technologies in Space-and Ground-based Telescopes and Instrumentation II, vol 8450. International Society for Optics and Photonics, p 84504K
3. Park K-S, Lee JH, Youn S-K (2005) Lightweight mirror design method using topology optimization. Opt Eng 44(5):053002
4. Doyle KB, Genberg VL, Michels GJ (2002) Integrated optomechanical analysis. vol 58. SPIE Press
5. Chan CY et al (2013) Design and analysis of isostatic mounts on a spaceborne lightweight primary mirror. In: Optomechanical engineering 2013, vol 8836. International Society for Optics and Photonics
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