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Physics Assignment: Conservation Laws, Orbits, and Black Holes, Exercises of Classical Physics

A physics assignment with problems related to conservation laws, orbital mechanics, and black holes. The problems involve calculating the speed of a satellite, the impulse required to put a spacecraft into an elliptical orbit around the sun, and the orbital period and mass of a binary star system. Students are expected to use the principles of conservation of energy and angular momentum, as well as newton's laws of motion.

Typology: Exercises

2011/2012

Uploaded on 08/12/2012

lalitchndra
lalitchndra 🇮🇳

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Download Physics Assignment: Conservation Laws, Orbits, and Black Holes and more Exercises Classical Physics in PDF only on Docsity! Due Wednesday, Nov 17, before 4 PM in 4-339B. This is not an easy assignment. You have 9 days; START EARLY! 8.1 Conservation Laws Imagine a spherical, non-rotating planet of mass M and radius R that has no atmosphere. A satellite is fired from the surface of the planet with speed v0 and at 20◦ to the local vertical. In its subsequent orbit the satellite reaches a maximum distance of 5R from the center of the planet. Calculate v0. 8.2 Much Ado About a Ham Sandwich You can find this problem in the Lecture Supplement (on the Home Page) of Nov. 3. This supplement gives you all the necessary background as discussed in lectures. 8.3 Going to the Sun A spacecraft of mass m is first brought into an orbit around the earth. The earth (together with the spacecraft) orbits the sun in a near circular orbit with radius R (R is the mean distance between the earth and the sun; it is about 150 million km). a) What is the speed of the earth in its orbit around the sun? We want the spacecraft to fall into the sun. One way to do this is to fire the rocket in a direction opposite to the earth’s orbital motion to reduce the spacecraft’s speed to zero (relative to the sun). b) What is the total impulse that would have to be given by the rocket to the spacecraft to accomplish this? You may ignore the effect of the earth’s gravitation as well as the orbital speed of the spacecraft around the earth as the latter is much smaller (how much smaller?) than the speed of the earth around the sun. Thus, you may assume that the spacecraft, before the rocket is fired, has the same speed in its orbit around the sun as the earth. We will now show that there is a more economical way of doing this (i.e., a much smaller rocket can do the job). By means of a brief rocket burn the spacecraft is first put into an elliptical orbit around the sun; the boost is provided tangentially to the earth’s circular orbit around the sun (see figure). The aphelion of the new orbit is at a distance r from the sun. At aphelion the spacecraft is given a backward impulse to reduce its speed to zero (relative to the sun) so that it will subsequently fall into the sun. c) Calculate the impulse required at the first rocket burn (the boost). d) What is the speed of the spacecraft at aphelion? docsity.com           boost fall into sun stop sun e) Calculate the impulse required at the second rocket burn (at aphelion). f) Compare the impulse under b) with the sum of the impulses under c) and e), and convince yourself that the latter procedure is more economical. g) Make a specific quantitative comparison for r = 20R. 8.4 Black hole in X-Ray Binary An X-ray binary consists of 2 stars with masses m1 (the accreting compact object) and m2 (the donor). The orbits are circular with radii r1 and r2 centered on the center of mass. a) Derive the orbital period of the binary following the guidelines given in lectures. b) In the case of Cyg X-1 (as discussed in lectures), the orbital period is 5.6 days. The donor star is a “supergiant” with a mass 30 times that of the sun. Doppler shift measurements indicate that the donor star has an orbital speed v2 of about 148 km/sec. Calculate r2. c) Calculate r1. Your calculations will be greatly simplified if instead of r1 you set up your equations in terms of r1/r2. Once you have solved for r1/r2, you have found r1 as you already know r2 (see part b). You will find a third order equation in r1/r2. Only one solution is real; the other two are imaginary. There are various ways to find an approximation for r1/r2. You can find the solution by trial and error using your calculator, or you can plot the function. d) Now calculate the mass m1 of the accreting compact object. As discussed in lectures, since this turns out to be substantially larger than 3 times the mass of the sun, it is strongly believed to be a black hole. 8.5 Rolling and Slipping Hoop – page 352, problem 45 8.6 Physical Pendulum – page 409, problem 34 8.7 Two Blocks, Two Slopes and a Pulley Two blocks m1 and m2 are connected by a light string (with negligible mass) passing over a pulley with mass M and radius R as shown. The pulley is a solid uniform disk, and the friction between it and the rope is such that when the blocks move the rope turns the pulley without slipping. The kinetic friction coefficient between the blocks and the slope is µ. Find the acceleration of the blocks, the angular acceleration of the pulley, and the tension in each part of the rope. Assume that m2 is much larger than m1 (the blocks go from left to right), and that the bearings of the pulley rotate without friciton.  M m m θ θ1 2 2 1 8.8 Doppler Effect I – page 462, problem 29 docsity.com
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