Power gen at high beta orbits (again, couple of times per year) is *significantly* reduced because of drag.
Like, it’s a huge deal.
Power gen at high beta orbits (again, couple of times per year) is *significantly* reduced because of drag.
Like, it’s a huge deal.
Starlink (yikes) works because it uses many cheap, expendable, redundant units and space is hard on everything.
Starlink (yikes) works because it uses many cheap, expendable, redundant units and space is hard on everything.
- ISS uses anhydrous ammonia (vs H2O) in its ATCS. Doesn’t freeze, great viscosity, similar thermal capacity, etc. Potential issue in hab modules but fine in practice over 30(?) yrs
- Notes on geo-sync orbit & latency, rocket costs are spot on. LEO vs Geo costs are non-trivial!
- ISS uses anhydrous ammonia (vs H2O) in its ATCS. Doesn’t freeze, great viscosity, similar thermal capacity, etc. Potential issue in hab modules but fine in practice over 30(?) yrs
- Notes on geo-sync orbit & latency, rocket costs are spot on. LEO vs Geo costs are non-trivial!