Abstract
The paper is aimed at obtaining the optimum mount configuration for a Zerodur primary mirror for a Cassegrain spaceborne electro-optical payload. A bipod flexure design procedure is presented while taking various optomechanical design principles into account. Finite element model of the flexure is established in ANSYS APDL to analyse the design w.r.t optical and mechanical design parameters. In the design process of the mounts, thickness of the flexure notches; angle between the bipods; and height of the mounts are optimized for the best optical performance.
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References
Kihm H, Yang H-S, Rhee H-G, Lee Y-W (2015) Development of 1-m primary mirror for a spaceborne camera. In: Optomechanical Engineering 2015, vol 9573. International Society for Optics and Photonics, p 95730W
Weingrod I et al (2013) Design of bipod flexure mounts for the IRIS spectrometer. In: Optomechanical engineering 2013, vol 8836. International Society for Optics and Photonics
Vukobratovich D, Coronato P (2015) Unit moment analysis as a guide to mirror mount design. In: Optomechanical engineering 2015, vol 9573. International Society for Optics and Photonics, p 95730R
Chu C et al (2011) Design of bipod flexures for space mirror. In: International symposium on photoelectronic detection and imaging 2011: space exploration technologies and applications, vol 8196. International Society for Optics and Photonics
Kihm H, Presenter H-SY, Moon I-K, Lee Y-W. Adjustable bipod flexures for mounting mirrors in a satellite telescope
Doyle KB, Genberg VL, Michels GJ (2002) Integrated optomechanical analysis, vol 58. SPIE Press
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
Daly JG, Daly DJ (2001) Structural adhesives for bonding optics to metals: a study of optomechanical stability. In: Optomechanical design and engineering 2001, vol 4444. International Society for Optics and Photonics, pp 177–185
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Tomar, S., Meena, B.R. (2020). Design of Primary Mirror Mount for Spaceborne EO Payload. In: Sastry, P.S., CV, J., Raghavamurthy, D., Rao, S.S. (eds) Advances in Small Satellite Technologies. Lecture Notes in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-15-1724-2_21
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DOI: https://doi.org/10.1007/978-981-15-1724-2_21
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