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A Multistage Rocket. Suppose the first stage of a two

University Physics | 13th Edition | ISBN: 9780321675460 | Authors: Hugh D. Young, Roger A. Freedman ISBN: 9780321675460 31

Solution for problem 113P Chapter 8

University Physics | 13th Edition

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University Physics | 13th Edition | ISBN: 9780321675460 | Authors: Hugh D. Young, Roger A. Freedman

University Physics | 13th Edition

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Problem 113P

A Multistage Rocket.? Suppose the first stage of a two stage rocket has total mass 12,000 kg, of which 9000 kg is fuel. The total mass of the second stage is 1000 kg, of which 700 kg is fuel. Assume that the relative speed ?v?ex of ejected material is constant, and ignore any effect of gravity. (The effect of gravity is small during the firing period if the rate of fuel consumption is large.) (a) Suppose the entire fuel supply carried by the two-stage rocket is utilized in a single-stage rocket with the same total mass of 13,000 kg. In terms of ?v?ex, what is the speed of the rocket, starting from rest, when its fuel is exhausted? (b) For the two-stage rocket, what is the speed when the fuel of the first stage is exhausted if the first stage carries the second stage with it to this point? This speed then becomes the initial speed of the second stage. At this point, the second stage separates from the first stage. (c) What is the final speed of the second stage? (d) What value of ?v?ex is required to give the second stage of the rocket a speed of 7.00 km/s?

Step-by-Step Solution:

Solution 113P Introduction In this problem we will use the equation of rocket motion to calculate the velocities. Step 1 We know that the change in the velocity of a rocket is given by Here And Hence, the change in velocity is Now since the rocket started from the rest, the velocity of the rocket when all the fuel is exhausted is

Step 2 of 4

Chapter 8, Problem 113P is Solved
Step 3 of 4

Textbook: University Physics
Edition: 13
Author: Hugh D. Young, Roger A. Freedman
ISBN: 9780321675460

The answer to “A Multistage Rocket.? Suppose the first stage of a two stage rocket has total mass 12,000 kg, of which 9000 kg is fuel. The total mass of the second stage is 1000 kg, of which 700 kg is fuel. Assume that the relative speed ?v?ex of ejected material is constant, and ignore any effect of gravity. (The effect of gravity is small during the firing period if the rate of fuel consumption is large.) (a) Suppose the entire fuel supply carried by the two-stage rocket is utilized in a single-stage rocket with the same total mass of 13,000 kg. In terms of ?v?ex, what is the speed of the rocket, starting from rest, when its fuel is exhausted? (b) For the two-stage rocket, what is the speed when the fuel of the first stage is exhausted if the first stage carries the second stage with it to this point? This speed then becomes the initial speed of the second stage. At this point, the second stage separates from the first stage. (c) What is the final speed of the second stage? (d) What value of ?v?ex is required to give the second stage of the rocket a speed of 7.00 km/s?” is broken down into a number of easy to follow steps, and 201 words. Since the solution to 113P from 8 chapter was answered, more than 396 students have viewed the full step-by-step answer. University Physics was written by and is associated to the ISBN: 9780321675460. This full solution covers the following key subjects: stage, speed, rocket, Fuel, mass. This expansive textbook survival guide covers 26 chapters, and 2929 solutions. The full step-by-step solution to problem: 113P from chapter: 8 was answered by , our top Physics solution expert on 05/06/17, 06:07PM. This textbook survival guide was created for the textbook: University Physics, edition: 13.

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A Multistage Rocket. Suppose the first stage of a two