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Question: At a certain instant of time mass of a rocket going up vertically is \[100\,{\text{kg}}\]. If it is ...

At a certain instant of time mass of a rocket going up vertically is 100kg100\,{\text{kg}}. If it is ejecting 5kg5\,{\text{kg}} of gas per second at a speed of 400m/s400\,{\text{m/s}}, the acceleration of the rocket would be (taking g=10m/s2g = 10\,{\text{m/}}{{\text{s}}^2})
A. 20m/s220\,{\text{m/}}{{\text{s}}^2}
B. 10m/s210\,{\text{m/}}{{\text{s}}^2}
C. 2m/s22\,{\text{m/}}{{\text{s}}^2}
D. 1m/s21\,{\text{m/}}{{\text{s}}^2}

Explanation

Solution

Use the formula for force acting on an object in terms of the linear momentum of the object. Use the formula for linear momentum of an object. Also use the expression for Newton’s second law of motion. We have given the rate of ejection of mass of the gas. Calculate the force acting on the rocket in upward direction due to ejection of gas. Also calculate the weight of the rocket. Calculate the net force on the rocket and then calculate the acceleration of the rocket.

Formulae used:
The force FF acting on an object is given by
F=dPdtF = \dfrac{{dP}}{{dt}} …… (1)
Here, dPdP is a change in momentum of the object in time dtdt.
The momentum PP of an object is
P=mvP = mv …… (2)
Here, mm is the mass of the object and vv is the velocity of the object.
The expression for Newton’s second law of motion is
Fnet=ma{F_{net}} = ma …… (3)
Here, Fnet{F_{net}} is net force acting on the object, mm is mass of the object and aa is acceleration of the object.

Complete step by step solution:
We have given that the mass of the rocket is 100kg100\,{\text{kg}}.
M=100kgM = 100\,{\text{kg}}
The rate of ejection of the mass of the gas from the rocket is 5kg5\,{\text{kg}} per second.
dmdt=5kg/s\dfrac{{dm}}{{dt}} = 5\,{\text{kg/s}}
We have also given that the velocity of the ejection of the gas from the rocket is 400m/s400\,{\text{m/s}}.
v=400m/sv = 400\,{\text{m/s}}
The gas ejecting out of the rocket gives an upward force to the rocket for its motion in the upward direction.
This force making the rocket to move in the upward direction is given by equation (1).
F=dPdtF = \dfrac{{dP}}{{dt}}
Substitute mvmv for PP in the above equation.
F=d(mv)dtF = \dfrac{{d\left( {mv} \right)}}{{dt}}
F=vdmdt\Rightarrow F = v\dfrac{{dm}}{{dt}}
Substitute 400m/s400\,{\text{m/s}} for vv and 5kg/s5\,{\text{kg/s}} for dmdt\dfrac{{dm}}{{dt}} in the above equation.
F=(400m/s)(5kg/s)\Rightarrow F = \left( {400\,{\text{m/s}}} \right)\left( {5\,{\text{kg/s}}} \right)
F=2000N\Rightarrow F = 2000\,{\text{N}}
Hence, the force acting on the rocket in the upward direction is 2000N2000\,{\text{N}}.
Let us now calculate the weight of the rocket in the downward direction.
W=MgW = Mg
Substitute 100kg100\,{\text{kg}} for MM and 10m/s210\,{\text{m/}}{{\text{s}}^2} for gg in the above equation.
W=(100kg)(10m/s2)W = \left( {100\,{\text{kg}}} \right)\left( {10\,{\text{m/}}{{\text{s}}^2}} \right)
W=1000N\Rightarrow W = 1000\,{\text{N}}
Hence, the weight of the rocket acting in the downward direction is 1000N1000\,{\text{N}}.
Let us now calculate the acceleration of the rocket.Hence, the net force acting on the rocket is
Fnet=FW{F_{net}} = F - W
Substitute FWF - W for Fnet{F_{net}} and MM for mm in equation (3).
FW=MaF - W = Ma
a=FWM\Rightarrow a = \dfrac{{F - W}}{M}
Substitute 2000N2000\,{\text{N}} for FF, 1000N1000\,{\text{N}} for WW and 100kg100\,{\text{kg}} for MM in the above equation.
a=(2000N)(1000N)100kg\Rightarrow a = \dfrac{{\left( {2000\,{\text{N}}} \right) - \left( {1000\,{\text{N}}} \right)}}{{100\,{\text{kg}}}}
a=10m/s2\therefore a = 10\,{\text{m/}}{{\text{s}}^2}
Therefore, the acceleration of the rocket would be 10m/s210\,{\text{m/}}{{\text{s}}^2}.

Hence, the correct option is B.

Note: The students should not forget to calculate the net force acting on the rocket as the force acting on the rocket is the vector addition of the upward force or thrust on the rocket and weight of the rocket in the downward direction. If this net forget is not calculated and only weight of the rocket is considered then we will end up with the incorrect value of acceleration of the rocket.