If
If ve and vo represent the escape velocity and orbital velocity of a satellite corresponding to a circular orbit of radius R, then
(a) ve = vo
(b) √2 vo = ve
(c) ve = v0/√2
(d) ve and vo are not related
Answer:b
(11)
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(a) – 5 J (b) – 10 J (c) – 15 J (d) – 20 J Answer-a (123)