Not really, the conversation began with the current plan of sending a nuclear reactor plus large tanks of liquid hydrogen to mars and wandered off from there,
The project you're talking about isn't a fusion reaction - it's a fission reactor being sent to split the water so that the shelf-stable water can be converted to rocket fuel in order to launch a sample return mission. It's not an efficient system, but it's nothing like traveller ships.
The energy released by fusion is about billions of times higher than the energy release by combustion.
A conventional rocket is throwing stuff out the back at high speed. Burning H2+O2 is the most energetic chemical reaction we know of, and it throws water out the back.
A normal Traveller space ship (which excludes TNE) throws nothing out the back, and uses hydrogen, it fuses it into helium, and uses gravitics to throw itself around. A 100 ton starship gets around at 1G with about 1 ton of PP.
ITER's reactor is expected to produce 500MW captured, with an energy cost to operate of 10MW, for a duration of 1000 sec on 0.5g of fuel per run. It should be running in 2019. So 490GW/Sec per 0.5g of fuel. And not all of that fuel is fused. But lets expand that to the 250MW Traveller drive. One ton is 1,000,000.g which gives 980,000,000,000.MW/Sec of recaptured power potentially. A day is 3600*24=86400s, and a week is 604,800sec. Given the output of 250 MW, a ton of fuel SHOULD produce 3,920,000,000sec at ITER efficiencies... or over 6400 weeks, or 125 years.... this means that the fuel rates in HG (as rated in MW by Striker) are about 1500x less efficient than the plant being built should be.