16
The preliminary layout of the ES housing consist of a common electronics box both
for LEO and GEO sensor, in front of an interchangeable LEO and GEO optical head.
Since LEO optical assembly dimensions are quite larger than GEO ones, the preliminary
housing layout has been dimensioned upon LEO optical assembly. Traditional materials
and production technologies shall be privileged thought the use of composites, in
particular carbon-fiber, for the optical housing may grant better structural performances.
Carbon-fiber optical housing could be a valid alternative to standard aluminum and shall
be considered in case of high overall weight due to aluminum use.
The selected preliminary configuration provides a common electronics enclosure both
for LEO and GEO sensor, in front of an interchangeable optical head. Thanks to this
solution the electronic board is the same both for LEO (Figure 18) and GEO (Figure19)
optics ensuring modularity and reliability. The bottom of the sensor act as interface with
the spacecraft providing power and data connector(s) and an additional electronics bay for
additional plug-in boards integration. Thus it is possible to increase sensor capabilities
simply by adding compatible interface, data elaboration and data storage units inside the
electronics bay.
Figure 18: LEO configuration
assembly
Figure19: GEO configuration assembly
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