Abstract
The mechanical structure and thermal system of the OBC was designed by the IRS. With this approach it was possible to find a configuration of the OBC housing and electronics as compact as possible and well adapted to the FLP target spacecraft.
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© 2013 Springer-Verlag Berlin Heidelberg
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Lengowski, M., Steinmetz, F. (2013). OBC Mechanical and Thermal Design. In: Eickhoff, J. (eds) A Combined Data and Power Management Infrastructure. Springer Aerospace Technology. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-35557-8_7
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DOI: https://doi.org/10.1007/978-3-642-35557-8_7
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Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-35556-1
Online ISBN: 978-3-642-35557-8
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