A rocket has to be launched from earth in such a way that it never returns. If E is the minimum energy delivered by the rocket launcher, what should be the minimum energy that the launcher should have if the same rocket is to be launched from the surface of the moon? Assume that the density of the earth and the moon are equal and that the earth's volume is 64 times the volume of the moon.
Alternate method: Escape velocity from earth's surface is given by, ve=√2GMR=√2GρVR =√2Gρ×4πR33R=√83πρGR2 Similarly, for moon, v′e=√83πρGR2m Now, volume of earth is 64 times volume of the moon. ⇒43πR3e=64×43πR3m ⇒ReRm=4 ∴v′e=√83πρG(R4)2=ve4 Now, EE′=12mv2e12mv′2e=v2ev′2c=v2e(v2e16)=16 ⇒E′=E16 |