Problem 20
Question
\(\bullet$$\bullet \mathrm{A} 75,600 \mathrm{N}\) spaceship comes in for a vertical landing. From an initial speed of \(1.00 \mathrm{km} / \mathrm{s},\) it comes to rest in 2.00 \(\mathrm{min}\) . with uniform acceleration. (a) Make a free-body diagram of this ship as it is coming in. (b) What braking force must its rockets provide? Ignore air resistance.
Step-by-Step Solution
Verified Answer
The braking force needed is approximately 11,366 N.
1Step 1: Draw the Free-Body Diagram
To draw the free-body diagram of the spaceship, identify all the forces acting on it during the vertical landing. There are two main forces: the gravitational force pulling the spaceship downwards (weight, denoted by \( F_g \)) and the braking force exerted by the rockets upwards (denoted by \( F_b \)). We can neglect air resistance as instructed. The diagram will show \( F_g = 75,600 \ N \) directed downward and \( F_b \) directed upward.
2Step 2: Determine Gravitational Force
The weight of the spaceship, which is its gravitational force, can be calculated using the given value: \( F_g = 75,600 \ N \). This is the downward force due to gravity.
3Step 3: Calculate Initial and Final Velocities
Convert the initial velocity from km/s to m/s for consistency. The initial velocity \( v_i = 1.00 \ km/s = 1000 \ m/s \). The final velocity \( v_f \) is 0 m/s since the spaceship comes to rest.
4Step 4: Calculate the Acceleration
Use the kinematic equation for uniform acceleration: \( v_f = v_i + at \). Rearrange this to solve for acceleration \( a \):\[ 0 = 1000 + a(120) \]\[ a = \frac{-1000}{120} \approx -8.333 \ m/s^2 \]We use 120 seconds for time since the time given is 2.00 minutes.
5Step 5: Use Newton's Second Law
According to Newton's second law, \( F_{net} = ma \). The net force \( F_{net} \) is the difference between the braking force \( F_b \) and the gravitational force \( F_g \) because they act in opposite directions:\[ F_{b} = F_{net} + F_{g} \]\[ F_{b} = ma + F_{g} \]
6Step 6: Determine Mass of the Spaceship
Calculate the mass using the gravitational force equation \( F_g = mg \). Rearrange it to find mass \( m \):\[ m = \frac{F_g}{g} = \frac{75600}{9.81} \approx 7708 \ kg \]
7Step 7: Calculate Braking Force
Substitute the known values into the equation for braking force:\[ F_{b} = 7708(-8.333) + 75600 \]\[ F_{b} = -64233.764 + 75600 \]\[ F_{b} \approx 11366 \ N \] \( F_b \) is positive because it acts in the opposite direction of \( a \).
Key Concepts
Free-Body DiagramUniform AccelerationNewton's Second LawBraking Force Calculation
Free-Body Diagram
A free-body diagram is a crucial tool in physics that helps us visualize the forces acting on an object. In the case of a spaceship coming in for a vertical landing, we focus on two main forces:
- Gravitational Force (Weight): This force pulls the spaceship downward towards the Earth. It is due to gravity and is calculated as the product of the mass and gravitational acceleration, given in the problem as 75,600 N.
- Braking Force: Acting upwards, this force is exerted by the rockets to counteract the pull of gravity and slow the spaceship down.
Uniform Acceleration
Uniform acceleration refers to the scenario where an object's velocity changes at a constant rate. In the exercise, the spaceship decelerates uniformly, meaning it comes to a stop following a steady decrease in velocity over time. This concept is essential when studying motion, as it allows us to use specific kinematic equations to solve for unknown variables like acceleration or final velocity.
In our context, the spaceship starts at an initial speed of 1.00 km/s, and comes to rest (0 m/s) in 120 seconds (2 minutes). To find the acceleration, we use the equation:
\[ v_f = v_i + at \]
Here, \( a \) is the uniform acceleration, \( v_f \) is the final velocity (0 m/s), \( v_i \) is the initial velocity (1000 m/s), and \( t \) is the time (120 s). Solving this gives \( a = -8.333 \, \text{m/s}^2 \). This negative sign indicates that the acceleration is in the opposite direction of initial velocity, i.e., it is a deceleration.
In our context, the spaceship starts at an initial speed of 1.00 km/s, and comes to rest (0 m/s) in 120 seconds (2 minutes). To find the acceleration, we use the equation:
\[ v_f = v_i + at \]
Here, \( a \) is the uniform acceleration, \( v_f \) is the final velocity (0 m/s), \( v_i \) is the initial velocity (1000 m/s), and \( t \) is the time (120 s). Solving this gives \( a = -8.333 \, \text{m/s}^2 \). This negative sign indicates that the acceleration is in the opposite direction of initial velocity, i.e., it is a deceleration.
Newton's Second Law
Newton's Second Law of Motion is a fundamental principle that describes how the motion of an object is affected by the forces acting upon it. It can be mathematically expressed as:
\[ F_{net} = ma \]
where \( F_{net} \) is the net force acting on an object, \( m \) is its mass, and \( a \) is the acceleration. In this problem, the net force is calculated as the difference between the upward braking force \( F_b \) provided by the spaceship's rockets, and the downward gravitational force \( F_g \).
When considering the spaceship:
\[ F_{net} = ma \]
where \( F_{net} \) is the net force acting on an object, \( m \) is its mass, and \( a \) is the acceleration. In this problem, the net force is calculated as the difference between the upward braking force \( F_b \) provided by the spaceship's rockets, and the downward gravitational force \( F_g \).
When considering the spaceship:
- Mass Calculation: The mass \( m \) can be derived from the gravitational force: \( F_g = mg \). By rearranging, \( m = \frac{F_g}{g} \), where \( g \) is the acceleration due to gravity (9.81 m/s²).
- Determining Braking Force: With the mass and acceleration known, we substitute into the equation: \( F_b = ma + F_g \), and solve for \( F_b \) to find the requisite braking force.
Braking Force Calculation
Calculating the braking force is central to ensuring that the spaceship comes to a complete and safe stop during its vertical landing. Using the formulas derived from the exercise, especially Newton's Second Law, we can compute the exact force needed from the spaceship's rockets.
First, we find the mass of the spaceship using the gravitational force:\
\[ m = \frac{F_g}{g} = \frac{75600}{9.81} \approx 7708 \, \text{kg} \]
Then, we plug the mass and the previously calculated deceleration into the net force equation. We express the braking force \( F_b \) as:
\[ F_b = ma + F_g \]
Substitute the values:
\[ F_b = 7708 \times (-8.333) + 75600 \]
\[ F_b = -64233.764 + 75600 \]
\[ F_b \approx 11366 \, N \]
This force is in the upward direction, counterbalancing gravity to bring the spaceship to rest. Calculating it accurately ensures the spaceship's safe landing by applying the right amount of thrust against gravity.
First, we find the mass of the spaceship using the gravitational force:\
\[ m = \frac{F_g}{g} = \frac{75600}{9.81} \approx 7708 \, \text{kg} \]
Then, we plug the mass and the previously calculated deceleration into the net force equation. We express the braking force \( F_b \) as:
\[ F_b = ma + F_g \]
Substitute the values:
\[ F_b = 7708 \times (-8.333) + 75600 \]
\[ F_b = -64233.764 + 75600 \]
\[ F_b \approx 11366 \, N \]
This force is in the upward direction, counterbalancing gravity to bring the spaceship to rest. Calculating it accurately ensures the spaceship's safe landing by applying the right amount of thrust against gravity.
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