Could I humbly ask that fuel and reaction mass be divided?
Reaction mass could simply be virtually anything your engine throws out the back. Obviously, engine designs will vary depending on the reaction mass used, so each engine design could have another line:
eg.
Reaction mass - H2O
Reaction mass - Inert Gas
This is a really good idea if you want to be realistic. Not so much because of the "different fuels" issue, but because of the interplay between engine mass, fuel mass, and reactor mass.
The way a reaction engine works is that you "burn" fuel in an engine to provide energy to throw "reaction mass" out the back end at some exhaust velocity to generate delta-momentum = mass thrown*velocity thrown. This is what's behind the fundamental difference between airplanes and rockets - the airplane doesn't have to carry its reaction mass - it uses its wings to thrown air downwards, and in the engine it uses the core to drive high-bypass fans to throw more air backwards more slowly than if the fans weren't there. If you go through the equations, this means that airplanes want LOW exhaust velocity, because that gets the most delta-momentum per delta-energy (fuel) (because kinetic energy = momentum^2/(2*mass)). Rockets, on the other hand, need to carry their reaction mass along with them, and pay for accelerating it before it's used. This causes reaction mass consumption to be exponential in the final velocity, btw, in the case where most of your ship is reaction mass. Since you're carrying the reaction mass along, you want to squeeze as much delta-momentum as possible out of each unit of it, so you want HIGH exhaust velocity. Rockets like a titan use combustion products as the reaction mass, while ion engines use a reactor or solar cells for the energy source and heavy ions as reaction mass. So there's a whole host of tech line possibilities:
* exhaust velocity
* fuel efficiency (how much energy is in one mass-unit of fuel)
* engine efficiency (how many mass units of engine it takes to process one mass-unit of fuel)
* fuel type (does the fuel get thrown overboard like rockets or kept on as deadweight e.g. reactor-mass, or is it solar powered)
One more thing to emphasize: if most of the mass of your ship is going to be fuel, you need to use the rocket equation, which says IIRC that the cost in reaction mass will be exponential, i.e. deltaV is something like log(TotalMassInitial/TotalMassFinal).
John