If ve and vo represent the escape velocity and orbital velocity of a satellite corresponding to a circular orbit of radius R respectively, then
(A) ve = vo
(B) \(\sqrt{2}\)vo = ve
(C) ve = \(\frac{1}{\sqrt{2}}\)vo
(D) ve and vo are not related
Answered Feb 05, 2023
Correct option is: (B) \(\sqrt{2}\)vo = ve
Correct Answer - `(a) 3.94xx10^(-4)H (b) 19.72xx10^(-3)V (c ) 19.72xx10^(-3)Wb//s (d) 9.86xx10^(-5)C`
Correct Answer - `30^(@), 0.866AU`
Correct answer is (D) 3 × 10+9 J
The minimum velocity with which a both’ should he thrown vertically upwards from the surface of the Earth so that it escapes the Earth ‘s gravitational field, is called the...
Correct Answer - (a) 3.1 km/s; (b) `-1/2`
Correct option is: (D) escape from the planet.
Correct option is: (B) \(2v_e\) Escape Velocity \(v_e = \sqrt {2gRe}\) \(\frac{V_{e1}}{V_{e2}} \propto \sqrt \frac{4R_1}{R_1}\) \(V_{escape \ 2} = 2 \ V_{escape \ 1}\)
Correct option is: (A) 11.2 km/s Escape velocity does not depend on the angle of projection. \(V_{escape} = \sqrt {2gRe} \)
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