|
Feb 22nd, 2021 at 2:58pm
Satellite internet downlink spot beam efficiency
The downlink power (watts) from a GEO orbit satellite is spread all over the beam coverage area, which is typically a whole continent or country, in the case of older satellites. This is fine for multi-destination broadcasting where there are many receive sites throughout the service area. In the case of internet access service the downlink carrier from the satellite has been giant high speed carriers (DVB-S2) carrying a stream of data packets to all customers and with the customer modem extracting only the data intended for them. Given the objective is to transmit each signal packet from the satellite to a specific earth station we really need one spot beam per customer. The smaller the diameter of the spot beams the better. Laser beams would be ideal!
At GEO height, to obtain high throughput (HTS), satellites need a large downlink antennas and higher frequencies like Ka band to produce small spots and even those spots are still quite large (0.5 deg diameter or 300km diameter, from height 38500km). . The use of low earth orbits (LEO) means less range for the beams to spread out, allowing tiny cell-sized spots to be created even at relatively 'low' frequncies like Ku band.
The initial v1 Starlink satellites use Ku band (10.7-12.7 GHz RHCP) for the downlink, using a phased array satellite antenna approx 0.6m square, to transmit multiple small spot beams. Each spot is only about 3 deg or 30km diameter, 550km height.
|