dtdM(t)=−bv2
in free space no external force so there in only thrust force on rocket
fin=dtdM(Vrel)
Ma=((t)−bv2)v
a=M(t)−bv3
A spaceship in space sweeps stationary interplanetary dust. As a result, its mass increases at a rate dtdM(t)=bv2(t), where v(t) is its instantaneous velocity. The instantaneous acceleration of the satellite is:
Held on 5 Sept 2020 · Verified 6 Jul 2026.
−bv3(t)
M(t)−bv3
−M(t)2bv3
−2M(t)bv3
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