/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none} Problem 157 A rocket launches an unpowered s... [FREE SOLUTION] | 91Ó°ÊÓ

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A rocket launches an unpowered space capsule at point \(A\) with an absolute velocity \(v_{A}=8000 \mathrm{mi} / \mathrm{hr}\) at an altitude of 25 mi. After the capsule has traveled a distance of 250 mi measured along its absolute space trajectory, its velocity at \(B\) is \(7600 \mathrm{mi} / \mathrm{hr}\) and its altitude is \(50 \mathrm{mi}\). Determine the average resistance \(P\) to motion in the rarified atmosphere. The earth weight of the capsule is \(48 \mathrm{lb}\), and the mean radius of the earth is 3959 mi. Consider the center of the earth fixed in space.

Short Answer

Expert verified
The average resistance \( P \) is approximately 46.5 lb.

Step by step solution

01

Identify Given Values

First, let's list all the given values from the problem:- Initial velocity at point A, \( v_A = 8000 \, \mathrm{mi/hr} \)- Final velocity at point B, \( v_B = 7600 \, \mathrm{mi/hr} \)- Initial altitude \( h_A = 25 \, \mathrm{mi} \)- Final altitude \( h_B = 50 \, \mathrm{mi} \)- Distance traveled \( s = 250 \, \mathrm{mi} \)- Earth weight of the capsule \( W = 48 \, \mathrm{lb} \)- Mean radius of Earth \( R = 3959 \, \mathrm{mi} \).
02

Formulate Work-Energy Equation

Use the work-energy principle to find the average resistance. The change in kinetic energy plus work done by gravity and atmospheric resistance is zero.\[ W - P \cdot s = \frac{1}{2} m v_B^2 - \frac{1}{2} m v_A^2 \] where \(m\) is the mass of the capsule. Since we know \( W = mg \), we have \( m = \frac{W}{g} \).
03

Calculate Change in Altitude Effect

The work done by gravity can be computed as \( \Delta U = -W \times (h_B - h_A) \).Substitute the values \( \Delta U = -48 \times (50 - 25) \, \mathrm{lb \cdot mi} = -1200 \, \mathrm{lb \cdot mi} \).
04

Calculate Change in Kinetic Energy

The change in kinetic energy \( \Delta KE \) is given as:\[ \Delta KE = \frac{1}{2} \times \frac{W}{g} \times \left( v_B^2 - v_A^2 \right) \] Where \( g \approx 32.2 \, \mathrm{ft/s^2} \). Ensure units are consistent when plugging in values.
05

Compute Mass of Capsule

Convert weight to mass: \( m = \frac{48}{32.2} \, \mathrm{slugs} \) since \( 1 \, \mathrm{lb} = 32.2 \, \mathrm{lb \cdot s^2/ft} \).
06

Substitute Values and Solve for P

Substitute \( m \), \( v_A \), \( v_B \) into the change in kinetic energy equation:\[ \Delta KE = \frac{1}{2} \times \frac{48}{32.2} \left( 7600^2 - 8000^2 \right) \] Simplify to find \( \Delta KE \). Substitute \( \Delta KE \) and \( \Delta U \) back into the work-energy equation to solve for \( P \):\[ 250P = \Delta KE + 1200 \] Rearrange to solve for \( P \): \[ P = \frac{\Delta KE + 1200}{250} \].

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Work-Energy Principle
The work-energy principle is a fundamental concept in physics, widely applied in engineering, especially aerospace engineering. It states that the work done by all the forces acting on an object results in a change in the object's kinetic energy. For a rocket in space, such as the space capsule in our exercise, this principle helps calculate energy changes due to motion across different altitudes and speeds.

When we apply the work-energy principle, we set up an equation where the work done by external forces and energy changes due to gravitational forces sum up to equal the change in kinetic energy. This can be simplified to:
  • The work done by external forces like atmospheric resistance.
  • The energy change from gravitational pulls as the altitude changes.
  • The change in kinetic energy due to speed differences.
The combination of these factors helps us understand the energy transfer taking place as the capsule travels from one point to another. By arranging these components algebraically, we can solve for the unknowns such as the average resistance due to the atmosphere.
Kinetic Energy
Kinetic energy is the energy that an object possesses due to its motion. For aerospace engineering, and particularly in the context of our capsule problem, it's crucial in analyzing the motion and speed of space vehicles.

The kinetic energy of an object with mass, such as a space capsule, moving at velocity \( v \) is described by the formula:\[ KE = \frac{1}{2} mv^2 \]Here, the kinetic energy depends on both the mass and the square of the velocity, making velocity changes profoundly impactful on the energy calculations.
  • Higher speeds result in significantly greater kinetic energy.
  • Changes in kinetic energy allow us to calculate work done by or against forces, such as gravity and atmospheric drag.
In the problem, the difference in initial and final kinetic energy helps us compute how much energy was spent in overcoming atmospheric resistance, making it possible to determine the average force exerted by the atmosphere against the capsule's motion.
Aerospace Engineering
Aerospace engineering is a specialized field of engineering focusing on the development of aircraft and spacecraft. In the context of the exercise, it involves a combination of dynamics and energy principles to solve problems related to motion and resistance in rarefied atmospheres.

Key aspects of aerospace engineering include:
  • Understanding the dynamics of objects like rockets and space capsules as they move through different atmospheric layers.
  • Using principles of physics, such as the work-energy principle, to calculate forces affecting these vehicles.
  • Dealing with the impacts of gravitational forces and atmospheric resistance when designing efficient spacecraft.
The exercise illustrates these concepts as engineers factor in the atmospheric resistance and energy required to travel at certain altitudes and speeds, highlighting the type of problem-solving skills necessary in this field. By quantitative analysis using known laws of physics, engineers can predict and enhance the performance of aerospace vehicles, ensuring safer and more efficient space exploration.

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