Physics, asked by manisha59, 1 year ago

what is the minimum energy required to launch a satellite of mass M from the surface of a Planet of mass M and radius R in a circular orbit at an altitude of 2r ?

Answers

Answered by jeenalBaindha
0

Answer:

Orbital velocity- Orbital velocity is the velocity at which a body revolves around the other body. The velocity of orbit depends on the distance between the object and the center of the earth. Hence, the minimum required energy is 5GmM6R.

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