Can a Rocket Reach the Sound Barrier Without Breaking Internal Equipment?

In summary, a 2.45×10^4-kg rocket with a 13.1-N instrument hanging from a wire that can support a maximum tension of 33.9N blasts off vertically from the Earth's surface with a constant acceleration. The minimum time for the rocket to reach the sound barrier without breaking the inside wire is unknown, as is the maximum vertical thrust of the rocket engines. The rocket's distance from the Earth's surface when it breaks the sound barrier is also unknown. The equations F = ma, w = ma, and vx = v0x + axt may be useful in finding a solution. The downward force acting on the rocket is calculated by multiplying the mass (24500 kg) by the gravitational
  • #1
monikraw
8
0

Homework Statement



A 2.45×10^4-kg rocket blasts off vertically from the Earth's surface with a constant acceleration. During the motion considered in the problem, assume that remains constant. Inside the rocket, a 13.1-N instrument hangs from a wire that can support a maximum tension of 33.9N .

Find the minimum time for this rocket to reach the sound barrier (330m/s) without breaking the inside wire.

Find the maximum vertical thrust of the rocket engines under these conditions.

How far is the rocket above the Earth's surface when it breaks the sound barrier?

Homework Equations



F = ma
w = ma
vx = v0x + axt

probably missing a couple

The Attempt at a Solution



The only thing I could think to do so far is to calculate the downward force acting on the rocket which would be weight?

so 24500 x 9.8 = 240100N acting downward

I don't know how to find the upward force.
I don't know what all this hanging instrument stuff is?

Help is much appreciated! Thanks c:
 
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  • #2
well so imagine you're dragging some object along a frictionless surface (say, ice) and you're pulling it with a rope

let's say you can accelerate at will (like you've got a jetpack on or something)

so when you're pulling this object along, it will experience a force, yeah?

Same idea here. The hanging instrument is being pulled upwards by the same force that is pushing the rocket up into the air.
 
  • #3
so the string can handle 2.587 times the force it's handling right now right? but how do I incorporate that into an equation to find speed or acceleration?
 
  • #4
the string can support 33.9N, and is feeling 13.1N when the system is at rest. How much more force can be applied before it breaks?
 
  • #5


As a scientist, it is important to approach a problem like this with a systematic and analytical mindset. The first step would be to identify and understand all the given information and variables in the problem.

In this case, we have a rocket with a mass of 2.45×10^4 kg, a maximum tension of 33.9 N for the wire, and a desired speed of 330 m/s. The acceleration of the rocket is constant and we are asked to find the minimum time, maximum vertical thrust, and distance from Earth's surface when it reaches the sound barrier.

To solve for the minimum time, we can use the equation v = v0 + at, where v is the final velocity, v0 is the initial velocity (which is 0 m/s), a is the acceleration, and t is the time. We know the final velocity is 330 m/s and the acceleration is constant, so we can rearrange the equation to solve for t. This gives us t = v/a = 330/9.8 = 33.67 seconds.

Next, to find the maximum vertical thrust of the rocket engines, we can use the equation F = ma, where F is the force, m is the mass, and a is the acceleration. In this case, the acceleration is also the same as the acceleration due to gravity, so we can use the weight of the rocket as the force. This gives us F = 2.45×10^4 kg x 9.8 m/s^2 = 240100 N. This is the maximum vertical thrust of the rocket engines.

To determine how far the rocket is from Earth's surface when it reaches the sound barrier, we can use the equation d = v0t + 1/2at^2, where d is the distance, v0 is the initial velocity, a is the acceleration, and t is the time. In this case, the initial velocity is 0 m/s and the acceleration is constant, so we can plug in the values we know to solve for d. This gives us d = 0 + 1/2 x 9.8 x (33.67)^2 = 5608.23 meters. Therefore, the rocket will be 5608.23 meters above Earth's surface when it reaches the sound barrier.

As for the hanging instrument, it is not relevant to the calculations, but it is important to consider in terms of the
 

FAQ: Can a Rocket Reach the Sound Barrier Without Breaking Internal Equipment?

What is rocket science?

Rocket science is a branch of engineering and physics that deals with the design, construction, and operation of rockets and spacecraft. It involves the study of propulsion systems, aerodynamics, and materials science to develop and improve rockets for space exploration and other applications.

What are the basic principles of rocket science?

The basic principles of rocket science include Newton's laws of motion, which state that for every action, there is an equal and opposite reaction. Rockets use this principle to generate thrust by expelling exhaust gases in the opposite direction of the desired movement. Other principles include aerodynamics, which is the study of how objects move through air and the principles of energy and momentum.

How do rockets work?

Rockets work by generating thrust from the combustion of propellant, which creates a force that propels the rocket in the opposite direction. The thrust is produced by a nozzle at the end of the rocket, which accelerates the exhaust gases and creates a high-pressure, high-velocity gas stream. The rocket also needs to overcome the force of gravity and air resistance to launch and move through the atmosphere.

What are the main components of a rocket?

The main components of a rocket include the payload, which is the object or equipment that the rocket is carrying, the propulsion system, which generates the thrust to move the rocket, and the guidance and control system, which directs and steers the rocket. Other components include the structure, fuel tanks, and engines.

What are the challenges of rocket science?

Rocket science presents many challenges, including the high cost and complexity of designing and building rockets, the extreme environments of space and atmospheric reentry, and the need for precise calculations and control systems. Other challenges include the development of lightweight and durable materials, as well as the safety and ethical considerations of space exploration.

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