Medium MCQ +4 / -1 PYQ · JEE Mains 2023

A space ship of mass $2 \times 10^{4} \mathrm{~kg}$ is launched into a circular orbit close to the earth surface. The additional velocity to be imparted to the space ship in the orbit to overcome the gravitational pull will be (if $g=10 \mathrm{~m} / \mathrm{s}^{2}$ and radius of earth $=6400 \mathrm{~km}$ ):

  1. A $7.9(\sqrt{2}-1) \mathrm{km} / \mathrm{s}$
  2. B $11.2(\sqrt{2}-1) \mathrm{km} / \mathrm{s}$
  3. C $7.4(\sqrt{2}-1) \mathrm{km} / \mathrm{s}$
  4. D $8(\sqrt{2}-1) \mathrm{km} / \mathrm{s}$ Correct answer

Solution

<p>To find the additional velocity required to overcome the gravitational pull and launch the spaceship into orbit, we first need to find the orbital velocity. The formula for orbital velocity (v) is given by:</p> <p>$v = \sqrt{\frac{GM}{r}}$</p> <p>where G is the gravitational constant, M is the mass of Earth, and r is the distance from the center of the Earth to the spaceship (which is the sum of the Earth&#39;s radius and the altitude of the spaceship&#39;s orbit).</p> <p>In this problem, the spaceship is orbiting close to Earth&#39;s surface, so we can approximate r as the Earth&#39;s radius. Given that g = 10 m/s² and Earth&#39;s radius R = 6400 km, we can relate the gravitational constant G and the mass of Earth M through the formula:</p> <p>$g = \frac{GM}{R^2}$</p> <p>Now, we can find the orbital velocity:</p> <p>$v = \sqrt{\frac{gR^2}{R}} = \sqrt{gR}$</p> <p>Converting the Earth&#39;s radius to meters:</p> <p>$R = 6400 \times 10^3 \mathrm{~m}$</p> <p>Plugging in the values:</p> <p>$v = \sqrt{10 \times 6400 \times 10^3} = 8 \times 10^3 \mathrm{~m/s}$</p> <p>Now, we need to find the additional velocity required to overcome the gravitational pull. To do this, we can use the formula for escape velocity:</p> <p>$v\text{escape} = \sqrt{2} \times v\text{orbital}$</p> <p>Finding the additional velocity required:</p> <p>$$\Delta v = v\text{escape} - v\text{orbital} = (\sqrt{2} - 1) \times v_\text{orbital}$$</p> <p>Plugging in the values:</p> <p>$\Delta v = (\sqrt{2} - 1) \times 8 \times 10^3 \mathrm{~m/s}$</p> <p>Converting the velocity to km/s:</p> <p>$\Delta v = (\sqrt{2} - 1) \times 8 \mathrm{~km/s}$</p> <p>Thus, the additional velocity required to overcome the gravitational pull and launch the spaceship into orbit is:</p> <p>$8(\sqrt{2}-1) \mathrm{~km/s}$</p>

About this question

Subject: Physics · Chapter: Gravitation · Topic: Kepler's Laws

This question is part of PrepWiser's free JEE Main question bank. 129 more solved questions on Gravitation are available — start with the harder ones if your accuracy is >70%.

Drill 25 more like these. Every day. Free.

PrepWiser turns these solved questions into a daily practice loop. Chapter-wise drills, full mocks, AI doubt chat. No auto-renew.

Start free →