- 8,943
- 2,955
DrStupid said:Why would you say that? Can you derive this equation from fundamental laws or definitions?
I would say so. Let me do a discrete approximation (which is appropriate, since matter is actually discrete).
So assume that you have a rocket of mass [itex]m_R[/itex] initially traveling at speed [itex]v_R[/itex] Some of the mass is made of fuel. Imagine a discrete amount of fuel [itex]\delta m[/itex] being burnt and thrown out the back at relative velocity [itex]v_{rel}[/itex] (this will actually be a negative value). Let [itex]\delta t[/itex] be the time interval for this process.
To avoid the controversial step of considering variable mass, I will consider this system to be composed of two objects with constant mass (at least during time interval [itex]\delta t[/itex]):
- A rocket of mass [itex]m_R - \delta m[/itex].
This has an initial velocity of [itex]v_R[/itex] and a final velocity of [itex]v_R + \delta v_R[/itex]. The change in momentum is [itex]\delta p_R = (m_R - \delta m)\ \delta v_R[/itex]. - A quantity of fuel of mass [itex]\delta m[/itex].
This has an initial velocity of [itex]v_R[/itex] and a final velocity of [itex]v_R + v_{rel}[/itex]. The change in momentum is [itex]\delta p_F = \delta m\ v_{rel}[/itex].
By conservation of momentum,
[itex]\delta p_R = -\delta p_F[/itex]
So
[itex]\delta p_R = -\delta m\ v_{rel}[/itex]
The average force on the rocket is [itex]\delta p_R/\delta t = -v_{rel}\ \delta m/\delta t[/itex].
In the continuum limit, [itex]F_R = - v_{rel} \dfrac{dm}{dt}[/itex]