tsiolkovsky's rocket equation question

K^2

[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.

K^2 Recognitions: Science Advisor	[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.