If $v_{e}$ is escape velocity and $v_{0}$ is orbital velocity of a satellite for orbit close to the earth's surface, then these are related by:

v_{0} = v_{e}

No worries! We‘ve got your back. Try BYJU‘S free classes today!

v_{e} = \sqrt{2 v_{0}}

No worries! We‘ve got your back. Try BYJU‘S free classes today!

v_{e} = \sqrt{2} v_{0}

Right on! Give the BNAT exam to get a 100% scholarship for BYJUS courses

v_{0} = \sqrt{2} v_{e}

No worries! We‘ve got your back. Try BYJU‘S free classes today!

Open in App

Solution

The correct option is C $v_{e} = \sqrt{2} v_{0}$

Suggest Corrections

Similar questions

V_{e}

V_{0}

v_{e}

v_{o}

v_{e}

v_{o}

v_{0}

v_{e}

If $v_{e}$ and $v_{o}$ represent the escape velocity and orbital velocity of a satellite corresponding to a circular orbit of radius R, then

Join BYJU'S Learning Program