A point $P$ lies on the axis of a ring of mass $M$ and radius $a$ at a distance $a$ from its centre $C$. A small particle starts from $P$ and reaches $C$ under gravitational attraction. Its speed at $C$ will be:
1. $\sqrt{\frac{2 GM}{a}}$
2. $\sqrt{\frac{2 GM}{a} \left(1 - \frac{1}{\sqrt{2}}\right)}$
3. $\sqrt{\frac{2 GM}{a} \left(\sqrt{2} - 1\right)}$
4. zero

A body of super dense material with mass twice the mass of the earth but size very small compared to size of the earth starts from rest from h<<R above the Earth's surface. It reaches earth in time t:

1. $t=\sqrt{\frac{h}{g}}$

2. $t=\sqrt{\frac{2h}{g}}$

3. $t=\sqrt{\frac{2h}{3g}}$

4. $t=\sqrt{\frac{4h}{3g}}$

Kepler's second law regarding constancy of the areal velocity of a planet is a consequence of the law of conservation of:

1. Energy

2. Linear momentum

3. Angular momentum

4. Mass

A projectile fired vertically upwards with a speed v escapes from the earth. If it is to be fired at 45$°$ to the horizontal, what should be its speed so that it escapes from the earth?

1.  v

2.  $\frac{\mathrm{v}}{\sqrt{2}}$

3.  $\sqrt{2}\mathrm{v}$

4.  2v

Magnitude of potential energy ($U$) and time period $(T)$ of a satellite are related to each other as:
1. $T^2\propto \frac{1}{U^{3}}$
2. $T\propto \frac{1}{U^{3}}$
3. $T^2\propto U^3$
4. $T^2\propto \frac{1}{U^{2}}$

Two bodies of masses m and 4m are placed at a distance r. The gravitational potential at a point on the line joining them where the gravitational field is zero is

1.  $-\frac{5\mathrm{Gm}}{\mathrm{r}}$

2.  $-\frac{6\mathrm{Gm}}{\mathrm{r}}$

3.  $-\frac{9\mathrm{Gm}}{\mathrm{r}}$

4.  0

If $A$ is the areal velocity of a planet of mass $M,$ then its angular momentum is:

In planetary motion, the areal velocity of the position vector of a planet depends on the angular velocity $(\omega)$ and the distance of the planet from the sun $(r)$. The correct relation for areal velocity is:
1. $\frac{dA}{dt}\propto \omega r$
2. $\frac{dA}{dt}\propto \omega^2 r$
3. $\frac{dA}{dt}\propto \omega r^2$
4. $\frac{dA}{dt}\propto \sqrt{\omega r}$

A projectile is fired upwards from the surface of the earth with a velocity $kv_e$ where $v_e$ is the escape velocity and $k<1$. If $r$ is the maximum distance from the center of the earth to which it rises and $R$ is the radius of the earth, then $r$ equals:
1. $\frac{R}{k^2}$
2. $\frac{R}{1-k^2}$
3. $\frac{2R}{1-k^2}$
4. $\frac{2R}{1+k^2}$

A satellite is moving very close to a planet of density $\rho.$ The time period of the satellite is:
1. $\sqrt{\frac{3 \pi}{ρG}}$
2. $\left(\frac{3 \pi}{ρG}\right)^{3 / 2}$
3. $\sqrt{\frac{3 \pi}{2 ρG}}$
4. $\left(\frac{3 \pi}{2 ρG}\right)^{3 / 2}$