The escape velocity for a rocket from the earth is \(11.2\) km/s. Its value on a planet where the acceleration due to gravity is double that on the earth and the diameter of the planet is twice that of the earth (in km/s) will be:
1. | \(11.2\) | 2. | \(5.6\) |
3. | \(22.4\) | 4. | \(53.6\) |
The escape velocity from the earth is about 11 km/second. The escape velocity from a planet having twice the radius and the same mean density as the earth is
1. 22 km/sec
2. 11 km/sec
3. 5.5 km/sec
4. 15.5 km/sec
What should be the velocity of earth due to rotation about its own axis so that the weight at equator become 3/5 of initial value. Radius of earth on equator is 6400 km
1. rad/sac
2. 6.4 rad/sac
3. rad/sac
4. 8.7 rad/sac
If g is the acceleration due to gravity at the earth's surface and r is the radius of the earth, the escape velocity for the body to escape out of the earth's gravitational field is:
1. gr
2.
3. g/r
4. r/g
The escape velocity of a projectile from the earth is approximately
1. 11.2 m/sec 2. 112 km/sec
3. 11.2 km/sec 4. 11200 km/sec
The escape velocity of a particle of mass m varies as:
1.
2. m
3.
4.
Acceleration due to gravity is ‘g’ on the surface of the earth. The value of acceleration due to gravity at a height of 32 km above earth’s surface is (Radius of the earth = 6400 km)
1. 0.9 g
2. 0.99 g
3. 0.8 g
4. 1.01 g
The time period of a simple pendulum on a freely moving artificial satellite is
1. Zero
2. 2 sec
3. 3 sec
4. Infinite
For the moon to cease as the earth's satellite, its orbital velocity has to be increased by a factor of:
1. | \(2\) | 2. | \(\sqrt{2}\) |
3. | \(1/\sqrt{2}\) | 4. | \(4\) |
The height of a point vertically above the earth’s surface, at which the acceleration due to gravity becomes \(1\%\) of its value at the surface is: (Radius of the earth = \(R\))
1. \(8R\)
2. \(9R\)
3. \(10R\)
4. \(20R\)