>It's interesting how further up someone accused people of opposing nuclear energy for ideological reasons and then read proposals like this, which are completely removed from reality.
Let's see. There are two variables here in regards to power subsystem: power and energy capacity. Let's start with the power:
>A container can weigh up to 28 tonnes, there was exactly one helicopter that could carry this kind of load the Mil Mi-12 and that looked really more like a plane.
According to ([1]), we need around 0.28 kW/kg of thrust. Assuming that the drone weights twice more than a container, we need to have a lift of around 84 tonnes-force minimum, and ~100 tonnes-force in reality. That translates to 0.28 * 10^5 kW = 28 MW. This is close to what Mi-12 had (19.2 MW).
LTO batteries from Toshiba ([2]) advertise 3.5 kW/kg of energy density, which gives us 28 MW/3.5 kW/kg = 800 kg of batteries. Reasonable, given that our budget for drone dry weight is 56 tonnes.
Let's consider the energy capacity. To transfer a container from one ship to another standing 200 meters apart moving at 10 km/h, we would need 144 seconds for roundtrip. Let's make it 300 seconds for redundancy.
28 MW * 300 seconds = 2333 kWh. At 84 Wh/kg ([2]), we get 27.8 tonnes of batteries. Not great, but within out weight budget of 56 tonnes.
The gotcha here that I see is the longevity of these batteries (they are rated for 8000 cycles). Do you see any other issues? I mean, basic physics seems to allow for such drones (not saying it's trivial to make).
1. https://store.tmotor.com/goods.php?id=974
2. https://www.electrive.com/2022/01/12/toshiba-presents-new-20...