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Tsiolkovsky's rocket equation question
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K^2
#
2
Nov26-12, 07:06 PM
Sci Advisor
P: 2,470
[itex]\Delta v[/itex] does not depend on thrust. Only on I
_{sp}
of the propellant. As long as I
_{sp}
is some constant, the [itex]\Delta v[/itex] will always be proportional to natural log of the mass ratio.