What are you using to calculate fuel usage, travel time, etc for interplanetary travel w the drives you mention? None of those will support the Traveller-standard aim-accelerate-flip-decelerate travel. Hohmann orbits are easy but slo-o-o-ow.
I use sub 1 G thrust and calculate the trips using fractional G's burning 1/2 the delta V in accel and half in decel, you are seriously underestimating the delta V available with a Fusion Rocket or a Daedalus drive.
The Fuel usage numbers given below are from T4 FF&S tables 163, 167, and 168.
Heplar .00125 m3/hr/KN Theroetical max accel 200 G's (666 KN/m3 fuel)
Thruster plate (PP fuel) Theroetical max accel 20 G's
Fusion Rkt .00035 m3/hr/KN Theroetical max accel 9 G's (2,857 KN/m3)
Ion .0002 m3/hr/KN Theroetical max accel .033G's (5,000 KN/m3)
Daedalus .00005 m3/hr/KN Theroetical max accel 1.5 G's (20,000 KN/m3)
*Theroetical max accel is engine only as it flings it's last dollop of fuel out the back, not counting any power sourses needed. (Thrust/engine mass)
Folks are used to seeing the Heplar drives used cause they're easy to make your ships reach 6 G's (takes about the same power as it does for J6), but the Fusion rocket uses 1/3 the fuel per KN/h and does not require seperate power input, and lastly the daedalus is a whopping 61 times less fuel per KN/h than the Heplar, and again no PP needed, and beats the Ion drive in fuel sipping.
A .15 g Daedalus installation takes about 10% of the ship's volume and mass, cost's an arm, leg, and three tentacles to install, but coupled to another 10% of the ship's volume in fuel can get you anywhere in the solar system within a few months at 20,000 KN per m3 of fuel.