The correct option is A 10 m/s2
Given,
Mass of the rocket = 2000 kg
Relative speed of gas ejected from the rocket
v=−100 m/s
(Taking downward direction -ve)
Rate of ejection of gas =400 kg/s=dMdt
As we know,
Ma=Fext+vdMdt=−Mg−vdMdt
⇒2000×a=−2000×10−(−100)×400
⇒a=10 m/s2