Chapter 6: Problem 723
What is the intensity of gravitational field at the center of spherical shell (A) \(\left(\mathrm{Gm} / \mathrm{r}^{2}\right)\) (B) \(\mathrm{g}\) (C) zero (D) None of these
Chapter 6: Problem 723
What is the intensity of gravitational field at the center of spherical shell (A) \(\left(\mathrm{Gm} / \mathrm{r}^{2}\right)\) (B) \(\mathrm{g}\) (C) zero (D) None of these
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Get started for freeThe largest and shortest distance of the earth from the sun are \(\mathrm{r}_{1}\) and \(\mathrm{r}_{2}\) its distance from the sun when it is at the perpendicular to the major axis of the orbit drawn from the sun (A) \(\left[\left(\mathrm{r}_{1}+\mathrm{r}_{2}\right) / 4\right]\) (B) $\left[\left(\mathrm{r}_{1} \mathrm{r}_{2}\right) /\left(\mathrm{r}_{1}+\mathrm{r}_{2}\right)\right]$ (C) \(\left[\left(2 r_{1} r_{2}\right) /\left(r_{1}+r_{2}\right)\right]\) (D) \(\left[\left(\mathrm{r}_{1}+\mathrm{r}_{2}\right) / 3\right]\)
A planet is revolving round the sun in elliptical orbit. Velocity at perigee position (nearest) is \(\mathrm{v}_{1} \mid\) and at apogee position (farthest) is \(\mathrm{v}_{2}\) Both these velocities are perpendicular to the joining center of sun and planet \(r\) is the minimum distance and \(\mathrm{r}_{2}\) the maximum distance. (1) when the planet is at perigee position, it wants to revolve in a circular orbit by itself. For this value of \(\mathrm{G}\) (A) Should increase (B) Should decrease (C) data is insufficient (D) will not depend on the value of \(\mathrm{G}\) (2) At apogee position suppose speed of planer is slightly decreased from \(\mathrm{v}_{2}\), then what will happen to minimum distance \(r_{1}\) in the subsequent motion (A) \(r_{1}\) and \(r_{2}\) both will decreases (B) \(\mathrm{r}_{1}\) and \(\mathrm{r}_{2}\) both will increases (C) \(\mathrm{r}_{2}\) will remain as it is while \(\mathrm{r}_{1}\) will increase (D) \(\mathrm{r}_{2}\) will remain as it is while \(\mathrm{r}_{1}\) will decrease
At what distance from the center of earth, the value of acceleration due to gravity \(g\) will be half that of the surfaces \((\mathrm{R}=\) Radius of earth \()\) (A) \(2 \mathrm{R}\) (B) \(\mathrm{R}\) (C) \(1.414 \mathrm{R}\) (D) \(0.414 \mathrm{R}\)
The height at which the weight of a body becomes \(1 / 16\) th its weight on the surface of (radius \(\mathrm{R}\) ) is (A) \(3 \mathrm{R}\) (B) \(4 \mathrm{R}\) (C) \(5 \mathrm{R}\) (D) \(15 \mathrm{R}\)
Given mass of the moon is \((1718)\) of the mass of the earth and corresponding radius is \((1 / 4)\) of the earth, If escape velocity on the earth surface is \(11.2 \mathrm{kms}^{-1}\) the value of same on the surface of moon is $=\ldots \ldots \ldots \ldots \mathrm{kms}^{-1}$. (A) \(0.14\) (B) \(0.5\) (C) \(2.5\) (D) 5
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