> jet fuel's USEFUL specific energy is more like 10-15MJ/kg due to needing to be burned.
New turbofans have efficiencies close to 50%, so it's more like 20 MJ/kg. Also, you need to take into account the prop efficiency for electric planes. Beyond Mach 0.5, the efficiency degrades very rapidly. So it's not just electric motor vs jet engine.
> more glider-like L/D of 25-35 (the best gliders can do 70).
This is not limited to electric planes. The reason no one has done it so far is the aeroelastic divergence.
> improved modern materials means you can just have most of your take-off mass be battery, compensating for the poorer specific energy
Again, this can be done for any aircraft, not just the electric ones.
> as low as 1200km is the minimum range needed for transatlantic flights
Do you really believe there is a market for 1200km hops at Mach 0.5. We already have ATR 72 and Bombardier Q400. Why no one is using them for long haul flight?