Posted by beavis on Wednesday, February 15, 2012 at 5:01pm.
You must have misspelled and omitted something.
I assume you mean pre-ignition mass, not per-ignition mass, which makes no sense.
If so, what is the pre-ignition mass? The number you have provided is a mass flow RATE.
The rocket lifts off then the trust equals the weight. Use the initial mass and the mass flow rate to figure out when that happens.
i haveeee!! ive posted the right question again please look it up again if you have time :(
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