Problem 77
Question
the task of designing an accelerometer to be used inside a rocket ship in outer space. Your equipment consists of a very light spring that is \(15.0 \mathrm{~cm}\) long when no forces act to stretch or compress it, \(\begin{array}{lllll}\text { plus } & \text { a } & 1.10 & \text { kg } & \text { weight. }\end{array}\) be attached to a friction- free tabletop, while the \(1.10 \mathrm{~kg}\) weight is attached to the other end, as shown in Figure 5.67 . (Such a spring-type accelerometer system was actually used in the ill-fated Genesis Mission, which collected particles of the solar wind. Unfortunately, because it was installed backward, it did not measure the acceleration correctly during the craft's descent to earth. As a result, the parachute failed to open and the capsule crashed on Sept. \(8,2004 .)\) (a) What should be the force constant of the spring so that it will stretch by \(1.10 \mathrm{~cm}\) when the rocket accelerates forward at \(2.50 \mathrm{~m} / \mathrm{s}^{2}\) ? Start with a free-body diagram of the weight. (b) What is the acceleration (magnitude and direction) of the rocket if the spring is compressed by \(2.30 \mathrm{~cm} ?\)
Step-by-Step Solution
VerifiedKey Concepts
Newton's Second Law
For example, in the spring accelerometer design exercise, the force exerted by the spring is calculated using this law. Here, the weight of the spring, which is 1.10 kg, experiences an acceleration due to the motion of the rocket. When the rocket accelerates forward, the spring force equals the product of mass and acceleration, providing a clear application of Newton's second law.
This direct relation ensures that we can predict how much force will be needed for a known mass and desired acceleration, a crucial component for designing systems to measure or respond to forces, such as an accelerometer in a rocket. It allows us to monitor changes in motion and understand dynamic systems effectively.
Free-Body Diagram
In the context of the spring accelerometer, the free-body diagram shows the forces on the 1.10 kg weight. There's a horizontal spring force acting on the weight when the rocket accelerates. Since the tabletop is frictionless, it simplifies the analysis by ensuring the spring force is the only horizontal force.
This visualization helps in systematically applying Newton’s Second Law. We see how the spring force opposes or aids the motion and how it relates to the changes in acceleration of the weight, providing insights into the mechanics of the entire system.
Hooke's Law
In the accelerometer design, Hooke's Law is essential for determining the spring constant \( k \), needed for specific displacement behavior. When calculating what spring constant would cause a 1.10 cm stretch at an acceleration of 2.50 m/s², Hooke's Law provides the framework. The earlier calculation of the spring force using Newton’s second law, 2.75 N, allows us to rearrange and solve \( k = \frac{F}{x} \). This process lets us tailor the spring to the application's specific needs, ensuring accurate measurements.
Similarly, when the spring is compressed, Hooke’s Law helps find the new force and consequently adjust to new conditions, essential for controlled environments like space missions.
Rocket Acceleration Analysis
When designing the accelerometer for a rocket, we examined both scenarios of the spring stretching and compressing. The direction and magnitude of these deformations indicate the rocket's motion status. If the spring stretches, it suggests forward acceleration, while compression hints at deceleration.
The exercise's initial calculation shows that a 1.10 cm displacement indicates acceleration at 2.50 m/s². Meanwhile, a 2.30 cm compression results in a calculation of 5.23 m/s². This methodical approach allows engineers to monitor a rocket's performance and adapt as necessary. This understanding of acceleration is crucial for safely navigating and controlling the rocket on its journey, emphasizing why tools like accelerometers are indispensable in aerospace technology.