CubeSpec is an ESA in-orbit-demonstration mission, based on a 12-unit CubeSat, that targets high-resolution astronomical spectroscopy. It is developed and funded in Belgium and scheduled for launch early 2026. The main parts of CubeSpec’s optical payload are an off-axis Cassegrain telescope, a high-resolution spectrograph, and a fine-guidance system. The primary mirror of the telescope has a rectangular shape, matched to the CubeSat form factor to maximise the aperture, covering approximately the surface area of two CubeSat units. The prism cross-dispersed echelle spectrograph delivers a spectral resolution of R = 55000 and covers the wavelength range from 420 to 620 nm in a single exposure. A fine steering mirror and a fine-guidance sensor provide accurate centering of the source image on the spectrograph slit to compensate for spacecraft pointing errors and jitter. Fitting these sub-systems inside the available payload volume (slightly more than 6U or half the spacecraft volume) made their optical design a technological challenge. To accommodate the large temperature excursions endured by the spacecraft during each orbit, the opto-mechanical design of both the telescope and the spectrograph is highly athermalised. In this contribution, we present the complete optical design as well as crucial aspects of the opto-mechanical design of the CubeSpec payload.


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    Title :

    CubeSpec optical payload



    Conference:

    Small Satellites Systems and Services Symposium (4S 2024) ; 2024 ; Palma de Mallorca, Spain


    Published in:

    Proc. SPIE ; 13546


    Publication date :

    2025-03-20





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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