Find the mass (m) of the rocket as a function of time, if it moves with a constant acceleration a in the absence of external force. The gas escapes with a constant velocity u relative to the rocket and its initial mass was m0.
A
m=m0e−at/u
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B
m=m0e−t/u
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C
m=m0eat/u
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D
m=m0e2at/u
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Solution
The correct option is Am=m0e−at/u
Since Fext=0, we get Fnet=Vr(−dmdt)=u−dmdt ... (I)
Also Fnet=ma ...(II)
By eq. (I) and (II) ma=−u⋅dmdt
Integrating, ∫mm0dmm=∫t0−adtu ⇒[lnmm0]=−atu ⇒mm0=e−at/u ⇒m=m0e−at/u