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  • Design and Testing of a Dual-Camera Payload for ESEO

    Paper number

    IAC-16,B4,4,3,x31978

    Coauthor

    Mr. Indrek Sünter, Tartu Observatory, Estonia

    Coauthor

    Mr. Henri Kuuste, Tartu Observatory, Estonia

    Coauthor

    Mr. Allan Kustavus, University of Tartu, Estonia

    Coauthor

    Mr. Ants Agu, Estonian University of Life Sciences, Estonia

    Coauthor

    Mr. Erik Ilbis, University of Tartu, Estonia

    Coauthor

    Mr. Georgi Olentšenko, Tartu Observatory, Estonia

    Coauthor

    Mr. Indrek Ploom, University of Tartu, Estonia

    Coauthor

    Mr. Jaanus Kalde, University of Tartu, Estonia

    Coauthor

    Mr. Jacob Luis López Seco, University of Vigo, Spain

    Coauthor

    Mr. Johan Kütt, Tartu Observatory, Estonia

    Coauthor

    Ms. Karoli Kahn, University of Tartu, Estonia

    Coauthor

    Mr. Paul Liias, Radius Space, Estonia

    Coauthor

    Dr. Riho Vendt, Tartu Observatory, Estonia

    Coauthor

    Mr. Samu-Pekka Ojanen, Tampere University of Technology, Finland

    Coauthor

    Mr. Sharad Chopra, University of Petroleum and Energy Studies, India

    Coauthor

    Mr. Silver Lätt, Tartu Observatory, Estonia

    Coauthor

    Mr. Sriram Hariharan, Luleå University of Technology, Sweden

    Coauthor

    Mr. Tõnis Eenmäe, Tartu Observatory, Estonia

    Coauthor

    Mr. Urmas Kvell, Tartu Observatory, Estonia

    Coauthor

    Mr. Viljo Allik, Tartu Observatory, Estonia

    Coauthor

    Dr. Andris Slavinskis, Tartu Observatory, Estonia

    Coauthor

    Dr. Mart Noorma, University of Tartu, Estonia

    Year

    2016

    Abstract
    Since 2012, European Space Agency (ESA), SITAEL and ten European universities have been developing the European Student Earth Orbiter (ESEO). The satellite bus is being designed, built and tested by SITAEL, whereas the payload modules are being developed by various universities throughout Europe. ESEO is a microsatellite to measure the radiation environment in Low Earth Orbit (LEO), test new technologies in space as well as take photos of Earth and other celestial bodies. The aim of the ESEO optical payload is to produce color images in the visible spectrum, mainly for public outreach purposes. Although, in addition to public outreach, the payload can also be used to monitor plankton blooms or changes in the polar ice caps.
    
    This paper presents the design, development and pre-launch testing of a lightweight and power-efficient dual-camera system for ESEO. The two-camera solution enables imaging of the same target with a different field of view. The wide angle camera provides context for telescopic images, making it easier to pinpoint the area that was photographed. The primary camera of the payload is a wide-angle camera based on the ESTCube-1 design with a $4.4~\mathrm{mm}$ telecentric lens, VGA CMOS color sensor and a $700~\mathrm{nm}$ IR cut-off filter. With a field of view of $46^{\circ} \times 35^{\circ}$, the ground resolution of the primary camera is around 1 km per pixel. The secondary camera is telescopic, has a Zeiss C Sonnar T* 1.5/50 lens, a $2592 \times 1944$ pixel CMOS color sensor and a Schott BG40 filter. With a field of view of $6.63^{\circ} \times 5^{\circ}$, the ground resolution of the secondary camera is about $20~\mathrm{m}$ per pixel. The payload features configurable internal image processing, progressive image compression and non-volatile storage. The resulting payload weighs about $800~\mathrm{g}$, on average consumes less than $560~\mathrm{mW}$ of power, with peaks up to $1.5~\mathrm{W}$. The payload is currently being tested and will be launched on ESEO at the end of 2016.
    Abstract document

    IAC-16,B4,4,3,x31978.brief.pdf

    Manuscript document

    IAC-16,B4,4,3,x31978.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.