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page 3 i'm going to need to wait a while to do this derivation. for one thing, it doesn't come out properly the way i'm currently approaching it. i'm not sure whether i need to introduce forces, or if i'm just not setting it up right. i'm also rusty as Fe2O3. however, the wonderful thing about the Web, being at the fairly mature stage it is, is that you can usually find what you need if you look around. the media lab at MIT has this derivation and a whole lot more. so i guess i can go brush up on things. also, their derivation includes the effect of gravity, which mine below does not. note the differences. in the meantime, i guess i'll just give you the result. i'll put a form below, also, so you can try a few computations yourself. remember: this formula assumes there are no outside forces -- no gravity, no wind resistance, nothing. this formula will work for a rocket in space far from any stars, planets, etc. to act on it with gravity. again, see the MIT derivation if you want the full picture. in the above equation: v is the rocket's final velocity, i.e. how fast it will go u is the velocity of the propellant leaving the rocket m0 is the inital mass of the rocket + fuel + payload (the mass at the start) m is the final mass, after fuel has been spent, stages have been dumped, etc. the largest rocket ever flown, the , the rocket that took us to the moon and back. |