mass fraction equation:
want to know for every 10k pounds of wet mass, what must be fuel. I put this in a spreadsheet before, but it is a hassle to go look for it again, so I have to derive it here for my purpose. Would like to know how much equipment you can land on Ceres based upon this. For example, if Ceres has delta v escape velocity of .51 km/sec, how much fuel are you going to need to land on it?
This thing destroyed my calculations that I just had here, so let's just state it simply like this. The moon requires about a pound of fuel to land a pound. With a much weaker gravitational field, you should be able to land on Ceres more than a pound for each pound of fuel. That means more equipment and so forth.
The derivation of the above equation gave me a number of ln( mass fraction ) = .0001. That seems to small of a number, so I may have screwed up.
Damn it all.
Update:
Yeah, that must have been an error. Anyway, I found the spreadsheet and its 13% fuel fraction if you use a methane / lox engine and its ISP is 380.
Update:
Looks like a Falcon Heavy could deliver a 1 ton payload, which is about the mass of the Curiosity Rover.
If you landed a Rover there, you could inspect for water sources with an eye towards a refueling station on the planetoid.
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