Choose the correct alternative.
1. | If the zero of potential energy is at infinity, the total energy of an orbiting satellite is negative of its kinetic energy. |
2. | If the zero of potential energy is at infinity, the total energy of an orbiting satellite is negative of its potential energy. |
3. | The energy required to launch an orbiting satellite out of earth’s gravitational influence is more than the energy required to project a stationary object at the same height (as the satellite) out of earth’s influence. |
4. | Both (1) and (3) are correct. |
A rocket is fired vertically with a speed of \(5\) km/s from the earth’s surface. How far from the earth does the rocket go before returning to the earth?
1. \(8\times10^6\) m
2. \(1.6\times10^6\) m
3. \(6.4\times10^6\) m
4. \(12\times10^6\) m
A spaceship is stationed on Mars. How much energy must be expended on the spaceship to launch it out of the solar system? (Mass of the space ship = 1000 kg; mass of the sun = 2× kg; mass of mars = 6.4× kg; radius of mars = 3395 km; radius of the orbit of mars = 2.28× km; G = 6.67×.)
1. 11 × 1010 J
2. 6 × 1011 J
3. 6.67 × 1010 J
4. 7.12 × 1011 J
A rocket is fired vertically from the surface of mars with a speed of 2 km/s. If 20% of its initial energy is lost due to martian atmospheric resistance, how far will the rocket go from the surface of Mars before returning to it?
(Mass of mars = 6.4× kg; radius of mars = 3395 km; G = 6.67× )
1. 477.2 km
2. 550.5 km
3. 493.9 km
4. 517.3 km