The ship engine converts fuel's energy into ship's kinetic energy and it needs 1 ton of fuel to accelerate to 1,000 miles/hour. To reach 2,000 miles/hour the engine needs 4 tons of fuel (4x kinetic energy at 2,000 compare to 1,000 miles/hour).
This is how cars work. By using the mass of the earth to push against, they can put nearly all the energy of fuel into kinetic energy of the car (ignoring drag).
But rockets don't work this way. Most of the energy from the fuel goes into kinetic energy of the exhaust. Only a small fraction goes into the energy of the vehicle. But as the burn goes on, the fraction goes up. So double the speed of the vehicle does not require double the fuel use.
The manager doesn't need to accelerate the capsule. The initial premise about needing 4x the fuel for double the speed is incorrect (for regular rockets). It might be possible if the ship isn't a rocket (maybe it's accelerating against a planet's powerful magnetic field). But that changes lots of things. Mainly what the speed of the craft is.
For a car, the ability to accelerate goes down as the thing you're pushing against (the ground) is moving faster. If your ship is pushing against something, then that's the speed that matters. The speed relative to the capsule is irrelevant.
Double speed means 4x kinetic energy. If all ship's kinetic energy comes from the fuel, 4x kinetic energy -> 4x fuel
There are at least 2 incorrect assumptions in that statement.
The first is that all the energy is going into the vehicle KE. That's not true. Some (actually, a lot) is going into the KE of the exhaust. Imagine this for how things are working:
- First second: 1000J fuel -> 1J KE rocket, 999J KE exhaust
- Second second: 1000J fuel -> 4J KE rocket, 996J KE exhaust
The second assumption is that the fuel has the same energy all the time. It has the same chemical energy all the time, but later on (same as "in a frame where the rocket has high forward velocity") it also has some KE. And it can give up that KE to give additional energy to the rocket.
The result of both is that as long as the rocket mass remains relatively constant, then the same fuel burn gives the same velocity change. In reality as the rocket loses mass, the same fuel burn will give more velocity (even though the vehicle is getting a much greater amount of energy in that frame).
This is completely OK due to conservation of energy, but you have to account for the KE of the fuel and the KE of the exhaust as well.