OK, here are some numbers to consider. I apologize in advance for the math/science lesson and the equations. For those that are not interested, skip to the table at the end...
Several things related to propulsion are tied up in the idea of Specific Impulse (Isp). Essentially it is a measure of how powerful your rocket is.
For example, liquid fuel rockets have an Isp of about 500, while the most advanced nuclear-electric rocket we can believably create has an Isp of about 100,000.
Another important concept, related to Isp is Exhaust Velocity (Vexh). This is the speed of the rocket stuff shooting out the back. The faster the exhaust, the more powerful the engine and the higher the Isp. Ironically, exhaust velocity also determines the fuel flow rate (FFR). The higher the exhaust velocity, the LOWER the FFR for the same thrust.
So, lets make some assumptions as see what happens.
1. Basic Rocket: If we assume that the fuel is liquid Hydrogen (LH2) then the Traveller displacement ton and the mass are the same (1 ton = 1Dton of LH2). We will also assume that the rocket as an overall density of LH2 for convenience.
2. Simple Math: While calculating fuel usage is an integration problem since as fuel is used the mass of the ship goes down etc etc... We will assume that the mass of the ship is essentially constant. This assumption is pretty good until our fuel volume exceeds about 50% of our ship mass. This is a CAUTION... the following calculations will NOT work when you calculated fuel needed exceeds about 50% of your ship mass.
3. Standard Ship: I will use a 100 ton ship (scout ship). All of the values given can be scaled linearly for any other mass of ship. If you want to figure the numbers for a 500 ton ship, multiply the fuel per hour by 5. Simple. Additionally, we will assume a 1g thrust. If you want higher thrust, multiply the fuel used by the the G value.
So, first some assumptions about future Fusion Drives. These are SWAGS (scientific wild ass guesses) that I have made trying to keep things semi-realistic. I have also tried to put things in Traveller TL terms. These are MY assumptions, YMMV.
Advanced Nuclear-Electric Propulsion (NEP) becomes available at TL 8. It is basically Nuclear Pulse Propulsion. The idea is that you take small nodules of hydrogen, zap them with a laser to cause fusion and kick the hot exhaust out the back for thrust. Exhaust velocity is about 1,000 kilometers per second (kps). These are numbers from real-world studies like the Orion project and the Daedalus Project.
Basic Fusion Drive (BFD) is available at TL 9, using gravitic focusing technology, exhaust velocities can be increased to about 1% speed of light (1%c) or 3,000 kps
Standard Fusion Drive (SFD) is available at TL 12 when microgravitic control is possible. This results in a 10 fold increase in exhaust velocity to 10%c (30,000 kps)
Advanced Fusion Drive (AFD) is TL 15 and increases exhaust velocity to 50%c (150,000 kps)
Very Advanced Fusion Drive (VFD) is TL 17 and assumes that the exhaust velocity is essential light speed (300,000 kps).
So, given these technologies and our standard ship at 1g acceleration, here are the estimated fuel consumptions:
Code:
Drive Vexh (kps) Isp (sec) FFR (tons/hr)
NEP 1,000 100,000 3.62
BFD 3,000 300,000 1.21
SFD 30,000 3,000,000 0.12
AFD 150,000 15,000,000 0.02
VFD 300,000 30,000,000 0.01
Now, to give you an idea of how much fuel it would take to travel to different planets, lets assume a constant acceleration at 1g (accelerate half way then decelerate at 1g the other half). For a trip to Mars the minimum distance is 0.5 AU, so lets use that as our starting point. At 1g, it will take about 24 hours to travel 0.5 AU. (Yes 1 day to Mars at 1g!)
Code:
Drive Fuel (Dtons)
NEP 86.9
BFD 29.0
SFD 2.9
AFD 0.6
VFD 0.3
Because of Assumption 2, the NEP numbers are NOT accurate, so these assumptions would not work for that drive at interplanetary ranges (you could use lower thrust ratings).
So, the Standard Fusion Drive would use 3 tons of fuel per day of thrust (1g). For the advance drive round it to 0.5 tons per day (why not?).
Assume the Fusion Drive has the same size and cost as the M-Drive in the TMB, ignore PP fuel and calculate M-Drive fuel based on how many days you want to be able to accelerate. You can use the travel times posted on other threads (or in the book) to determine how far you can travel in a given time at a given acceleration. This WILL increase your fuel, but not really that much. Now instead of spending 2 tons of fuel per drive letter for PP fuel for 2 weeks, you spend 3 tons of fuel per ship size letter for 1 day of acceleration at 1g. Many of the standard designs could probably be left alone and just convert the PP fuel to Mdrive fuel and calculate the new endurance.
This is all done with a lot of assumptions, but should give people that want to have realistic reaction drives in their TU a way to calculate M-Drive fuel pretty easily
Fuel = (Ship Size/100)*Thrust (in Gs)*Days of Thrust*3