Correct Answer - Option 4 : 1 ∶ 2
The correct answer is option 4) i.e. 1 ∶ 2
CONCEPT:
-
Escape velocity is the minimum velocity with which a body is projected from the surface of the planet so as to reach infinity, by overcoming the pull by gravity.
Escape velocity at the surface of a planet is given by:
\(⇒ V_e=\sqrt{\frac{2GM}{R}}\)
Where G = gravitational constant (6.67 × 10-11 Nm2/kg2), M = mass of the planet and R = radius of the planet.
- The time period of a satellite: It is the time taken by the satellite to complete one revolution around the Earth.
Consider a satellite orbiting the earth at a height h from the surface of the earth of radius R.
The circumference of orbit of satellite = 2πR
The
orbital velocity of the satellite is given by:
\(⇒ v_0 =\sqrt{\frac{GM}{R}}\)
EXPLANATION:
- Given that the planets are similarly sized i.e. they have the same radii (R).
- Let the mass of the two planets be M1 and M2 and the acceleration due to gravity be g1 and g2 respectively.
- The escape velocity = orbital velocity
⇒ Ve = vo
\(⇒ \sqrt{\frac{2GM_1}{R}}=\sqrt{\frac{GM_2}{R}}\) ---(1)
-
Acceleration due to gravity g is obtained from balancing the equation of force with the equation of gravitational force.
\(mg =\frac{GMm}{R^2}⇒ g =\frac{GM}{R^2}\) ---(2)
Where M is the mass of the earth, m is the mass of an object, R is the radius of the earth, and G is the gravitational constant.
Substituting (2) in (1),
\(⇒ \sqrt{\frac{2g_1R^2}{R}}=\sqrt{\frac{g_2R^2}{R}}\)
\(\Rightarrow \frac{g_1}{g_2} = \frac{1}{2}\)