there's probably no great need to shorten trip time for cargo, so it can probably be close to a basic TMI of 4 km/s or so (varying by synod). Say 5 km/s.. if exhaust velocity = 3600 m/s (since they need SL Raptor for gimballing) then that's a mass ratio of right about 4. If a Mars ship is 120 tons dry mass + 100 tons payload, that's 660 tons propellant - if v4 tankers manage 200 tons, that's only four tankers (so if it's $5M/launch, $25M/out bound ship).If the delta-V needed is closer to 4 km/s, three tankers (and $20M/out bound ship)..
I started doing the math in the BO section "plans" thread - can it really be only 3 or 4 tankers per Marsbound ship?Quote from: Vultur on 11/16/2025 05:26 pm there's probably no great need to shorten trip time for cargo, so it can probably be close to a basic TMI of 4 km/s or so (varying by synod). Say 5 km/s.. if exhaust velocity = 3600 m/s (since they need SL Raptor for gimballing) then that's a mass ratio of right about 4. If a Mars ship is 120 tons dry mass + 100 tons payload, that's 660 tons propellant - if v4 tankers manage 200 tons, that's only four tankers (so if it's $5M/launch, $25M/out bound ship).If the delta-V needed is closer to 4 km/s, three tankers (and $20M/out bound ship)..3 to 1 probably won't work since some extra propellant is needed for the landing burn on Mars.Still, a 4 to 1 ratio seems exceptionally good.