Let (Vo) and (V.) represent the orbital velocity and escape velocity o

1.	Let (Vo) and (V.) represent the orbital velocity and escape velocity of a satellite corresponding to a circular orbit of radius R. Derive the relation between them.
Answer» ANSWER: Correct OPTION is B v e = 2 v o ESCAPE velocity v e = GM/R ORBITAL velocity v o = GM/2R so, v e = 2 v o

Let (Vo) and (V.) represent the orbital velocity and escape velocity of a satellite corresponding to a circular orbit of radius R. Derive the relation between them.

Answer»

ANSWER:

Correct OPTION is

ESCAPE velocity v

GM/R

ORBITAL velocity v

GM/2R

so, v

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Let (Vo) and (V.) represent the orbital velocity and escape velocity of a satellite corresponding to a circular orbit of radius R. Derive the relation between them.​

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Let (Vo) and (V.) represent the orbital velocity and escape velocity of a satellite corresponding to a circular orbit of radius R. Derive the relation between them.