Nilesat 102: Difference between revisions

It was manufactured by the European company [[Matra Marconi Space]] ([[Astrium]]). At launch, the spacecraft weighed 1,827&nbsp;kg (fully fuelled). The receiver dish diameter is 50 cm to 75 cm. The transponder output power is 100 W and the12 Ku-band transponders with a bandwidth isof 33 MHz. The maximum power consumption is 3.06 kW.<ref name="techinfo">{{cite web|url=http://www.nilesat.com.eg/Satellite/NileSat102/TechnicalInformation.aspx|title=Technica Information|website=Nilesat|access-date=November 6, 2016}}</ref> The satellite is powered by two deployable solar arrays, with the power being stored on batteries.<ref name="gunter" />