Trust me, it will when you have a whole ship meshed out and you find out it's all wrong. :dry:
I assume we're still using hydrogen for fuel, so the tanks indeed have to be cryogenic. That's a problem that never occured to me.
Actually when you get up to the maximum exhaust velocity you can get out of a fusion reaction, you'll pretty much be using the fusion fuel as propellant (as I understand it). Atomic Rockets has an
interesting table detailing the exhaust velocities possible with several different fusion reactions.
Proton-Proton fusion has the highest exhaust velocity of the lot- 11.7% of c, but fusing four protons together is nigh impossible. He3-D is a good option, but there will still be neutron-emitting side reactions. He3-He3 is entirely aneutronic (though I think I might have heard that it spits out a gamma ray once in a while), but requires more He3 and is harder to achieve than He3-D fusion (at least, it's harder to do than He3-D fusion, I don't know if it approaches p-B11 fusion in difficulty).
The kind of fusion drives I've desperately been trying to understand over the last few months are ones that inject hydrogen propellant into the plasma resulting from fusion or somehow otherwise use a fusion reaction to heat propellant. This increases thrust at the expense of exhaust velocity, and decreases efficiency, but also (unless I'm horribly, horribly incorrect here) decreases the amount of expensive fusion fuel needed.
Here you will need to use fusion fuel as propellant- you will need thousands of tons of fusion fuel. But interstellar spaceflight is not cheap. At least this fusion propellant is cheaper than antimatter.
In addition, since we want high thrust (the higher the thrust, the shorter the transit time), we're probably gonna have to go with something like Daedalus; inertial confinement fusion (my limited understanding tells me that ICF gets a higher thrust/mass due to not requiring the heavy magnets of a tokamak, or something like that).
Daedalus is the only concept that comes anywhere close to having a high thrust/mass ratio.
This article describes some of the aspects of the Daedalus propulsion system.
This page also contains some interesting information pertaining to fusion propulsion. Just to highlight the power/mass and thrust/mass problems; with a spheromak with a specific power of 10.5 kW/kg, you would still need an engine massing 3800 tons for only a 40 gigawatt engine; clearly impractical.
I've even read that it might even be possible- using extremely powerful capacitors to initiate fusion- to build an IC drive with a T/W of over 1. But ICF propulsion still has problems; for example, pellet design, pellet storage, pellet transport to the engines, laser/particle beam emitter design, throttling, pulse rate, and dealing with the effects of vibration on the vehicle and its occupants.
But that fusion fuel will likely still need to be kept at cryogenic temperatures.
If you're using an antimatter beam-core drive, your matter fuel will likely be in the form of LH2. The antimatter, however, is an entirely different story. And if you're using something like Orion, your pulse units will not be stored in tanks at all, but rather in gigantic propellant magazines, feeding pulse units to the detonation point in a manner at least vaguely similar to a rifle feeding rounds into the chamber for firing.
Of course, the optimal drive here would be something that gets 0.25 c, 0.3 c exhaust velocity, is capable of high acceleration, requires minimal fuel, and does not require large amounts of antimatter. I don't know what that would be. Even a proton-proton drive, with a mass ratio of 20, could only get up to 35% of c (not counting relativistic effects), enough to get to Alpha Centauri in roughly 12 years, only enough to get to Gliese 581 in roughly 50 years ship-time.
Handwavion-catalyzed fusion, maybe? :facepalm: