Re: Tinfoil Hats?
Please keep in mind I was replying to a post which suggested that the majority of the 400 tons of water was for shielding and only a small amount of that would be needed as propellant: see my emphasis below. (p.s. I haven't checked the feasibility of Voland's right hand's proposal so I admit I am making one assumption there by accepting the hand's suggestion). This is important because it means much less than 400 tons would be needed to be lifted from Earth to LEO to be used as propellant.
The only way to provide reasonable shielding is if the astronauts are shielded by the propellant. 1m of water goes a very long way towards shielding both nuclear propulsion and cosmic rays. 1m tank + shield around a sphere with 10m radius is ~ 400 tons. If some of this water is used as a propellant to get to Mars orbit and back you are also looking at a journey time under 30 days.
It is a lovely chart, yes I've seen it before, and thanks for reminding me of it. What the chart shows is that the Δv needed to get from LEO to Mars (9.51) is pretty much the same as the Δv needed to get from Earth to LEO (9.4). So, it's do-able. Especially if Voland's right hand is correct and the propellant needed to go from LEO to Mars and back is only a small part of the 400 tons of water.