Satellite with variable master cross section
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United States of America Patent
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Apr 17, 2018
Grant Date -
Jan 7, 2016
app pub date -
Jul 2, 2015
filing date -
Jul 4, 2014
priority date (Note) -
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status (Latency Note)
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Abstract
A satellite comprises at least one first communication module, a repeater module, one or more antennas, at least one propulsion module and an avionics module, the repeater module comprising: a north first panel when the satellite is in an orbital position, an east second panel, a south third panel and a west fourth panel arranged respectively opposite the north first panel and the east second panel, the north panel and the south panel having widths XmcR in the east-west direction, the east panel and the west panel having a width or YmcR in the north-south direction; characterized in that: the value of the ratio XmcR/YmcR for the repeater module lies within the interval [0.84; 1.12], and the repeater module consists of a number of floors, and the value of Xmck varies as a function of the floor k and of its position in the repeater module.
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