Enoki
SOC-14 1K
One Kilowatt is equal to 3414 BTUs, and one BTU is equal to approximately 778 foot-pounds. Assuming not-quite perfect efficiency, then figure that one Kilowatt will lift 3,000 pounds to 750 feet above ground level on Earth. With an Air/Raft massing, loaded, at 8 metric tons or 17,636.981 pounds, to lift an Air/Raft to 750 feet will take about 6 Kilowatts. For every additional 750 feet, another 6 kilowatts will be required.
The forward speed of an Air/Raft is given at 100 Kilometers per hour, with some capable of 120 kilometers per hour, so about 62 to 75 miles per hour. That is about the top speed of some of the early biplanes, with a lot of drag producing wires, struts, and landing gear. The biplanes needed about 100 or so horsepower to achieve that speed. The Air/Raft might have a bit more frontal area for drag, so you might need somewhere around 150 or so horsepower to move it. One kilowatt is equal to 1.34 horsepower, assuming perfect efficiency. Allowing for inefficiency and drag, I will assume that an Air/Raft will need 150 to 200 kilowatts of power for forward motion.
It would appear that an Air/Raft will need a power plant capable of generating at least 24 kilowatts of power for every 900 meters of altitude capability, and at least 200 kilowatts for forward power. Drag will be less in thinner air and greater in denser air, so performance may vary based on the planet's atmosphere. For a 9000 meter altitude capability at 120 kph, it will require about 440 kilowatts of power. If you divert power from the forward propulsion plant to altitude, you can, of course, go higher.
I think it'd take a bit more than that.
For example, a Beechcraft Baron twin engine light aircraft (~2,000 kg) has a power output of 388 KW. It cruises at about 200 mph. It also generates its lift from the wings almost entirely. That is, it cannot climb vertically overcoming its own weight using the engines. Its stall speed is about 85 mph. I'm not sure how much power is required to maintain at least 85 mph but it would certainly be a small fraction of that its capable of generating.
But, it is also obvious that it needs most or all of that 388 KW to get airborne and up to speed.
With an air raft the vehicle has to generate sufficient acceleration, at a minimum to rise at 9.8m a second or about 35 Kilometers an hour (say 22 mph) right off just to oppose gravity on Earth. For 8 metric tons to rise at all requires about 79 (MV) metric tons per second of acceleration. That works out to about 78 KW just to get that weight off the ground and keep it there.
Now we need to get it moving forward at say 100 kph / 60 mph. Guesstimating drag and what not, and allowing for reasonable acceleration based on our airplane, lets say it takes a third of what the plane does. After all, the loaded air raft is nearly four times as heavy loaded but is only trying to go about a third as fast and most acceleration is a square function depending on how its being done. I think 100 KW is reasonable.
So, to give a bit of extra umpf here, let's say 200KW is necessary, at a minimum and with inefficiencies and a safety factor let's say 300 KW. Now, if the top speed were around 100 mph you'd need somewhere around 600 to 800 KW as a first approximation.
One thing is clear, the energy to overcome gravity is not insignificant and it is more efficient for a aircraft to have a higher speed since that doesn't require nearly as much energy as simply overcoming gravity.
Such a craft could run on a gas turbine or some future power plant but internal combustion isn't going to hack it.