MCQ
A spaceship in space sweeps stationary interplanetary dust. As a result, its mass increases at a rate $\frac{ dM ( t )}{ dt }= bv ^{2}( t ),$ where $v ( t )$ is its instantaneous velocity. The instantaneous acceleration of the satellite is
- A$-\frac{2 b v^{3}}{M(t)}$
- B$-\frac{ bv ^{3}}{2 M ( t )}$
- C$-b v^{3}(t)$
- ✓$-\frac{b v^{3}}{M(t)}$

