Here is my list of Maneuver Drives, these drives are also power plants of the same type, they can either deliver 1 EP of energy or 50 tons of thrust per unit.
Maneuver Drives
Type_________________ TL Size____ Cost____ Fuel Usage
Fission (50 tons)____ 7_ 2 tons__ Mcr 6___ 2.9 tons/min
Fusion (50 tons)_____ 9_ 1.5 tons Mcr 4.5_ 7 tons/hour
Fusion (50 tons)_____ 13 1 ton___ Mcr 3___ 3.5 tons/hour
Fusion (50 tons)_____ 15 1 ton___ Mcr 3___ 0.18 tons/hour
Fusion (50 tons)_____ 16 1 ton___ Mcr 3___ 0.09 tons/hour
Antimatter (50 tons)_ 17 1 ton___ Mcr 1___ 0.015 tons/day antimatter + 0.015 tons/day hydrogen
I got these figures by consulting "The StarFlight Handbook" Chapter 3 Rocket Propulsion for Interstellar Flight.
Using the formula:
Delta-V = Exhaust-V ln (original_Mass / final Mass)
I used these given figures for specific impulse:
Solid Core Fission = 1000 sec -> exhaust Velocity = 10,000 m/sec
Fusion ranged from 2500 sec to 200,000 sec impulse so I divided it up into 4 parts assigning
Fusion TL 9 = 25,000 Sec -> 250,000 m/sec
Fusion TL 13 = 50,000 Sec -> 500,000 m/sec
Fusion TL 15 = 100,000 sec -> 1,000,000 m/sec
Fusion TL 16 = 200,000 Sec -> 2,000,000 m/sec
The Antimatter rocket was a pion drive with 50% efficiency, in my calculation I assumed total conversion to deterimine the amount of mass that needed to be converted into energy, and that is the total usage of antimatter required, but since the conversion is only 50% efficient, the rocket requires an equal amount of matter in the form of hydrogen to be used up at the same rate as the antimatter. The exhaust velocity in this calculation is the speed of light since light is its exhaust.
After determining the final velocity of each rocket type with an initial mass of 50 tons and a final mass of 49 tons, I assumed that each rocket type can produce 50 tons of force per unit, that is my handwave, but it is a lesser handwave than assuming gravitic technology. Inertial confinement fusion can achieve greater thrust than known magnetic confinement fusion, but perhaps some future technology would solve this problem and just use liquid hydrogen as fuel instead of pellets or bombs, so the spaceship can skim a gas giant for fuel. Hydrogen pellets or bombs can't be skimmed out of gas giant atmospheres and have to be manufactured, so I'm assuming that somehow you can get 50 tons of force out of a 1 ton fusion rocket. With that handwave I offer you these alternatives to traditional Traveller maneuver drives. If you want 1-g of acceleration simply add enough rocket units so that the force generated equals the starship's hull tonnage and we'll assume that the starship's average density is equal to that of liquid hydrogen. To get higher that 1 g acceleration add enough units so that the force generated is equal to a multiple of the hull tonages. These rockets are also power plants and each unit can also supply 1 EP to the ships systems if its rocket fuction is turned off, the rocket then simply contains the reaction and extracts energy from it. A scout ship would need 4 rocket units for instance to have 2-g acceleration, if the scout ship accelerated at only 1-g, it would use 2 units as rockets and would have 2 additional rocket units avialable as power plants able to supply 2 EP to the ship for weapons or whatever else. A dedicated power plant can also be included in adition to that. The rocket units require no energy inputs from the powerplant to operate. When the rocket units are rockets they have a greater fuel consumption than when they are used as power plants. When using the rockets as power plants, use the same rates of fuel consumption as the dedicated power plants in the T20 book.
Hows That?