Physics — Rocket & Variable Mass
Thrust and the Tsiolkovsky rocket equation.
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F = v_e\frac{dm}{dt}
\Delta v = v_e\ln\frac{m_0}{m_f}
a = \frac{v_e}{m}\frac{dm}{dt} - g
\text{thrust} = \dot{m}\,v_e
Thrust and the Tsiolkovsky rocket equation.
F = v_e\frac{dm}{dt}
\Delta v = v_e\ln\frac{m_0}{m_f}
a = \frac{v_e}{m}\frac{dm}{dt} - g
\text{thrust} = \dot{m}\,v_e