To reach the moon requires - By chemical rocket: 1000 tons of chemical fuel for each 1 ton of payload with 1000:1 ratio roughly linear with increasing payload. Max capability today is on order of 100 tons per launch. - By nuclear detonations: fuel:payload closer to 3:1 with prototype design of 400 ton payload for single rocket, and later designs aiming for 100,000 ton payload/rocket.
Is 30x less waste by mass better even if that waste is in part radioactive? Water waste still seems pretty good to me.
https://newatlas.com/orion-project-atom-bomb-spaceship/49454...