Firstly, I would like to say good job for making one of these. The SARP has a need for a rapid-transit vehicle. Beat me to it.
In regards to passenger capacity, I don’t think even 4,000 passengers is that much out of whack. A 747-400 carries 530 passengers and is, by volume, somewhere in the range of 1/15th the size of this vehicle. The biggest issue with thousands of passengers is that you will spend far longer loading and unloading people then you will to get to your destination.
However, some of Uso’s other concerns /are/ valid.
For the power, since we are using what are essentially BS technologies for FTS travel with no real connection with actual science it is impossible to derive valid power figures for their use. As a result I can’t argue that its impossible to use fusion to power a FTL system, but I do say that it is not a ideal power method. Compared to M-AM power systems it produces less than 1/100th the theoretical energy output (i.e. the best-case scenario, ignoring any inefficiencies) per unit mass of fuel. Aether and other quantum-effect power systems (Hyperspace tap, CDDA, etc.) exceed the capabilities of any fuel-based system by orders of magnitude when looked at from a power-to-mass and power-to-volume perspective. Because of this, I would expect a rather large amount of internal space to be taken up by the things power systems to enable it to use such a subpar method to power FTL.
In regards to fuel, I would agree that it is problematic to hold that much fuel on the vehicle. To use some IRL examples, surface ships warships use a considerable amount of their internal volume to hold the fuel necessary for a months-long cruise and receive in-trip refueling during these. Modern cargo and cruise ships use far less space, but they only carry enough fuel for a handful of months travel (many times much less) since they are going to and from built-up ports where refueling is easily available. It just wouldn’t make sense for them to carry 6 months of fuel when the longest trip they can reasonably expect to take is only going to be 6-7 weeks. A modern jetliner carries enough fuel for 8 hours on the upper end so that they can make transoceanic flights. Most carry far less. It doesn’t make sense for them to haul around the extra weight of several trips worth of fuel when they can easily pick it up when they land.
Similar logistics would apply to your ship. It is going from populated, industrialized worlds to other populated, industrialized worlds. Also realize that even a long trip is not going to go much over two hours with its FTL speed. Considering these two it makes no sense for it to carry a years worth of fuel. Heck, it wouldn’t make much sense for it to carry more than a days fuel. Anything beyond that is cutting in to space that could be used for paying customers.
From a technical standpoint, it also presents problems. As a first, you are carrying the fuel in a incredibly inefficient form. The part of the heavy-water you want is the deuterium or tritium (It should be noted here that these are isotopes of hydrogen, containing a extra one and two neutrons per atom respectively. Heavy water does not contain a extra hydrogen atom as the submission suggests. T wouldn’t be water if it did. Also be aware that tritium is radioactive with a half-life of ~12 years.). These make up somewhere between 1/8th (only one deuteride atom per molecule) to 1/2.7th (two tritium atoms per molecule) of the total fuel mass. The rest of that mass (all the oxygen and normal hydrogen) is wasted mass. This is exacerbated by the fact that water is pretty much incompressible, so even with supertech its is still going to take up a lot of space. A far, far more efficient method to transport it would be to extract the deuterium or tritium (whichever one you are using in this design) and freeze it to a slush state. This would massively increase the ratio of fuel to mass.
Even with that part of the issue solved, you will still have problems with the shear mass of fuel you would need for a years travel. For any reaction engine (be it a ion drive, a rocket engine, or a ship propeller) you need to accelerate a mass one direction to get the engine to go the other way, requiring both a input energy and a input mass. On a nuclear surface ship it only needs to carry the first of these, the input energy. The mass involved is surrounding it as the ocean. It doesn’t expend any mass, volume, or energy to carry this with it, it will be wherever the ship operates. Aircraft have the same advantage, only needing to carry the fuel to heat the air the jet engines expel.
A space ship, regardless if it is using a kerosene/O2 rocket, a ion drive, or a nuclear fusion torch, doesn’t have that advantage. It must carry both the input mass and energy. As a result they are vastly less efficient in regards to thrust produced compared to engine mass (including fuel). You simply can’t compare any space-based reaction drive with one within a massive media (be it air or water).
Lastly, the amount of acceleration needed to reach .15c in anything like a useful time frame for a vessel that crosses a light year in two minutes is going to be in the thousands (it would take it 15 minutes to reach that speed at 5,000Gs) which is not low in any sense. Nor is a top speed of 45,000 km/s. Within the context of the setting they are not terribly abnormal, but they are by no means low.
All of these things point toward the same conclusion, together and as a whole, that this ship would need a huge amount of internal space devoted towards its fuel. Assuredly more than its passenger capacity.
This brings us back to the first point.
Why would they waste so much space on fuel?
Its meant to operate within the sphere of modern space, where fuel is plentiful and easily available, why waste all that potentially profit-making space on heavy fuel? It just doesn’t make sense.