If -v-e- is escape velocity and -v-o- is orbital velocity of a satellite orbit close to the earth-s surface- then these are related by -v-o-v-e-v-e-sqrt -2-v-o-v-e-sqrt -2-v-o-v-o-sqrt -2-v-e-

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Toppr Admin · Accepted Answer

Vescape-x221A-2GMRvorbital-x221A-GMRvescape-x221A-2vo

If $v_{e}$ is escape velocity and $v_{o}$ is orbital velocity of a satellite for orbit close to the earth's surface, then these are related by :
$v_{o} = v_{e}$
$v_{e} = \sqrt{2 v_{o}}$
$v_{e} = \sqrt{2} v_{o}$
$v_{o} = \sqrt{2} v_{e}$

$v_{e s c a p e} = \sqrt{\frac{2 G M}{R}}$
$v_{o r b i t a l} = \sqrt{\frac{G M}{R}}$
$v_{e s c a p e} = \sqrt{2} v_{o}$

If ve is escape velocity and vo is orbital velocity of a satellite for orbit close to the earth's surface, then these are related by :vo=veve=√2vove=√2vovo=√2ve

vescape=√2GMRvorbital=√GMRvescape=√2vo

If $v_{e}$ is escape velocity and $v_{o}$ is orbital velocity of a satellite for orbit close to the earth's surface, then these are related by :
$v_{o} = v_{e}$
$v_{e} = \sqrt{2 v_{o}}$
$v_{e} = \sqrt{2} v_{o}$
$v_{o} = \sqrt{2} v_{e}$

$v_{e s c a p e} = \sqrt{\frac{2 G M}{R}}$
$v_{o r b i t a l} = \sqrt{\frac{G M}{R}}$
$v_{e s c a p e} = \sqrt{2} v_{o}$