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A novel deployable telescope to facilitate a low-cost <1m GSD video rapid-revisit small satellite constellation

Authors :
Roy Blows
Martin J. Booth
Jason Shore
Karen M. Hampson
Guy Richardson
Andrew Haslehurst
David Smith
Guglielmo S. Aglietti
Chris Saunders
David Gooding
Source :
Gooding, D, Richardson, G, Haslehurst, A, Smith, D, Saunders, C, Aglietti, G, Blows, R, Shore, J, Hampson, K & Booth, M J 2019, A novel deployable telescope to facilitate a low-cost <1m GSD video rapid-revisit small satellite constellation . in Proceeding of SPIE 11180, International Conference on Space Optics — ICSO 2018 . https://doi.org/10.1117/12.2535928
Publication Year :
2019
Publisher :
SPIE, 2019.

Abstract

The multi-billion dollar Earth observation applications market continues to demand better spatial and temporal resolution; simply put, this means bigger apertures and more satellites. This paper describes a novel deployable telescope that addresses the market needs for a Surrey Satellite Technology Ltd. (SSTL) has already demonstrated low-cost 1m GSD imagery from the Carbonite-2 platform, but the deployable telescope solution presented here provides the opportunity to build on this capability by significantly improving revisit time, without the typical increase in cost. SSTL is developing, alongside the Surrey Space Centre (SSC) and the Dynamic Optics and Photonics Group at the University of Oxford, a telescopic deployable structure and a fine alignment system to align the Cassegrain-type telescope in-orbit. The three-concentric barrel deployable structure and mechanisms are discussed including the associated requirements and trade-off study that led to this design. The dynamic nature of this system exacerbates traditional optical challenges such as alignment and stray light control; solutions to these are proposed, the optical design rationale is explained and predicted imaging performance shown. The novel autonomous fine alignment system, both algorithms and mechanisms, is presented. The last section deals with the spacecraft level implications and accommodation. Then finally the constellation level system design is shown with regards to the launch vehicle options and orbit configuration for coverage optimization; both global and target-specific.

Details

Database :
OpenAIRE
Journal :
International Conference on Space Optics — ICSO 2018
Accession number :
edsair.doi.dedup.....707a94db5e362febffcc1330df5bb80a
Full Text :
https://doi.org/10.1117/12.2535928