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> just a simple question please, dfd
helokit
Posted: Feb 1 2006, 07:14 AM


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A 4000 kg rocket is to be accelerated at 4.0g at take-off from the Earth. If the gases can be ejected at a rate of 20 kg/s, what must be their exhaust speed?

Is 4.0g the acceleration or is it 4.0*9.8. can you please tell me how to start solving this problem please
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Moseley
Posted: Feb 1 2006, 01:00 PM


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Yes 4.0g =4*9.8
There is a section on rocket propulsion in the pinned thread at the top of this board, the whole of which you should read regularly.
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