A body is projected vertically upwards from the surtace of a planet of radius \(\mathrm{R}\) with a velocity equal to half the escape velocity for that planet. The maximum height attained by the body is $\ldots \ldots \ldots \ldots$ (A) \((\mathrm{R} / 3)\) (B) \((\mathrm{R} / 2)\) (C) \((\mathrm{R} / 4)\) (D) \((\mathrm{R} / 5)\)

Short Answer

Expert verified
The maximum height attained by the body is \(H = R\), which corresponds to option (B).

Step by step solution

01

Write down the known parameters

The radius of the planet is R. The initial velocity (v0) is equal to half the escape velocity, which is given by the formula: \(v_e = \sqrt{\frac{2GM}{R}}\), where G is the gravitational constant, and M is the mass of the planet. So, the initial velocity v0 is: \(v_0 = \frac{1}{2}v_e = \frac{1}{2}\sqrt{\frac{2GM}{R}}\)
02

Apply the conservation of mechanical energy

We can write the total mechanical energy of the system (kinetic energy + gravitational potential energy) at launch (initial) and at the maximum height (final). Initially, the projectile has kinetic energy and potential energy due to its position on the planet's surface: \[E_{initial} = \frac{1}{2}mv_0^2 - \frac{GMm}{R}\] At the maximum height (H), the projectile's velocity is 0 (it momentarily stops moving upwards), so its kinetic energy is 0. However, it has potential energy due to its position at height H: \[E_{final} = -\frac{GMm}{R+H}\] Since the mechanical energy is conserved, we can write: \[E_{initial} = E_{final}\]
03

Solve for the maximum height H

From the energy conservation equation, we get: \[\frac{1}{2}mv_0^2 - \frac{GMm}{R} = -\frac{GMm}{R+H}\] Substitute the initial velocity v0 into the equation and solve for the unknown height H: \[\frac{1}{2}m\left(\frac{1}{2}\sqrt{\frac{2GM}{R}}\right)^2 - \frac{GMm}{R} = -\frac{GMm}{R+H}\] Simplify and solve for H: \[\frac{1}{4}\frac{2GMm}{R} - \frac{GMm}{R} = -\frac{GMm}{R+H}\] \[-\frac{1}{2}\frac{GMm}{R} = -\frac{GMm}{R+H}\] Cancel out the negative signs and GMm, and cross-multiply: \[\frac{1}{2R}(R+H)=1\] Solve for H: \[H = R\left(\frac{1}{\frac{1}{2}} - 1\right) = R\left(2-1\right) = R\] Therefore, the maximum height attained by the body is \(H = R\), which corresponds to option (B).

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with Vaia!

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

The maximum and minimum distance of a comet from the sun are $8 \times 10^{12} \mathrm{~m}\( and \)1.6 \times 10^{12} \mathrm{~m} .$ If its velocity when nearest to the sun is \(60 \mathrm{~ms}^{-1}\), What will be its velocity in \(\mathrm{ms}^{-1}\) when it is farthest? (A) 6 (B) 12 (C) 60 (D) 112

What is the intensity of gravitational field at the center of spherical shell (A) \(\left(\mathrm{Gm} / \mathrm{r}^{2}\right)\) (B) \(\mathrm{g}\) (C) zero (D) None of these

If \(\mathrm{V}_{\mathrm{e}}\) and \(\mathrm{V}_{\mathrm{o}}\) are represent the escape velocity and orbital velocity of satellite corresponding to a circular orbit of -adius \(\mathrm{r}\), then A) \(\mathrm{V}_{\mathrm{e}}=\mathrm{V}_{\mathrm{o}}\) (B) \(\sqrt{2} \mathrm{~V}_{\mathrm{o}}=\mathrm{V}_{\mathrm{e}}\) C) \(\mathrm{V}_{\mathrm{e}}=\left(\mathrm{V}_{\mathrm{O}} / \sqrt{2}\right)\) (D) \(\mathrm{V}_{\mathrm{e}}\) and \(\mathrm{V}_{\mathrm{o}}\) are not related

Match the following Table-1 \(\quad\) Table-2 (A) kinetic energy (P) \([(-\mathrm{GMm}) /(2 \mathrm{r})]\) (B) Potential energy (Q) \(\sqrt{(\mathrm{GM} / \mathrm{r})}\) (C) Total energy (R) - [(GMm) / r] (D) orbital velocity (S) \([(\mathrm{GMm}) /(2 \mathrm{r})]\) Copyright (O StemEZ.com. All rights reserved.

A planet moving along an elliptical orbit is closest to the sun at a distance \(\mathrm{r}_{1}\) and farthest away at a distance of \(\mathrm{r}_{2}\). If \(\mathrm{v}_{1}\) and \(\mathrm{v}_{2}\) are the liner velocities at these points respectively, then the ratio \(\left(\mathrm{v}_{1} / \mathrm{v}_{2}\right)\) is \(\ldots \ldots \ldots \ldots\) (A) \(\left(\mathrm{r}_{1} / \mathrm{r}_{2}\right)\) (B) \(\left(\mathrm{r}_{1} / \mathrm{r}_{2}\right)^{2}\) (C) \(\left(\mathrm{r}_{2} / \mathrm{r}_{1}\right)\) (D) \(\left(\mathrm{r}_{2} / \mathrm{r}_{1}\right)^{2}\)

See all solutions

Recommended explanations on English Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.

Sign-up for free