- #1
enfield
- 21
- 0
How would the equation look if instead of knowing the effective exhaust velocity we knew the force the exhaust was exerting on the rocket.
The equation is:
[tex] \Delta V = v_e * ln(\dfrac{m_0}{m_1}) [/tex]
would [tex] \Delta V [/tex] still be proportional to the log of the initial mass over the final mass?http://en.wikipedia.org/wiki/Tsiolkovsky's_rocket_equation
The equation is:
[tex] \Delta V = v_e * ln(\dfrac{m_0}{m_1}) [/tex]
would [tex] \Delta V [/tex] still be proportional to the log of the initial mass over the final mass?http://en.wikipedia.org/wiki/Tsiolkovsky's_rocket_equation