|
|
|
|
|
by elihu
1285 days ago
|
|
I would expect L1-to-earth communication to be problematic because you'd have to distinguish the signal from the background radiation of the sun. It'd be interesting to know what the technical limits are in terms of output power and aim/focus. Generally, doubling distance means the signal power drops to 1/4th, and maximum data capacity of a communication link is proportional to the signal/noise ratio. So that would mean a 100 Gbps link might drop to 25 Gbps. You might be able to bring the signal/noise ratio back up by using a better detector or a more powerful laser, or aiming better. Or maybe the 100 Gbps data rate is limited by the transceiver, and there's actually plenty of S/N ratio margin that can be traded for range without affecting data rate at all. |
|
However, the problem is not quite as bad as it seems. Spacecraft at L1 and L2 Lagrange points actually are in a halo orbit that "orbits" around the Lagrange point. Attempting to stay at exactly the L1 or L2 point is unstable, since gravitational forces tend to knock you away from that point. The halo orbits are much more stable. And for a spacecraft in a halo orbit, you never have to point your antenna directly at the sun.
The problem is solvable for radio communication at least. There are currently 4 spacecraft orbiting the Earth-Sun L1 point (ACE, DSCOVR, SOHO, and WIND) as well as 3 spacecraft at the L2 point (Gaia, James Webb, and Spektr-RG).