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Post by zorbeltuss on Jun 30, 2017 1:22:34 GMT
So I did calculations on Thrust/Cost and probably someone else would be interested too, the engines I used was made to give an ideal value, stoichiometric ratio of 1 if applicable Nozzle expansion of 1000 and a pump radius of 10 cm, otherwise it's just the ordinary "New Combustion Rocket Module" engine and will not hold up to the rigors of real life. Mass Ratio is taken directly out of the game except for the ones specified in this thread Mass ratio and Mass flow wierdness. It can be imported into google docs, but I don't want to fiddle with it because I have a fever and should probably go to sleep. It is also not likely to be updated by me but you're free to improve and update, fix and share it if you want. CoaDE fuel calc.ods (20.52 KB)
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