Solving Rocket Launch at 75 Degrees After 11.2s

In summary, to find the location of the rocket after 11.2 seconds, you will need to use the equation d = vt + (1/2)at^2, where v is initial velocity, t is time, and a is acceleration. You can break the acceleration into its x and y components and use the given values to calculate the x and y distances. Keep in mind that the acceleration in the x direction is not affected by gravity, while the acceleration in the y direction is the difference between the original acceleration and gravity.
  • #1
HomerPepsi
1
0

Homework Statement


A rocket is launched at an angle of 75 degrees and accelerates at 21.4 m/s^2. Where is the rocket located (from the point of origin) after 11.2 seconds?

Homework Equations


a=(vf - vi) / t

(vf + vi) / 2 = (xf - xi) / t

where: vf = velocity final, vi = velocity initial, xf = displacement final, xi = displacement initial, and of course a = acceleration and t = time

The Attempt at a Solution


given solution: Xfx = 353.7 m; Xfy = 693.4 m (don’t forget gravity in the y-direction)

X
ax = 21.4cos75 = 5.54
vix = vi cos75
vfx= vi cos75
xfx = ?
xix = 0
t = 11.2

Y
ay = 21.4sin75 = 20.67
viy = vi sin75
viy = ?
xfy = ?
xiy = 0
t = 11.2

any one got any Ideas to the path to the solution, and how do i account for gravity? add/subtract?

thanks
 
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  • #2
I believe your main problem is that you don't have the equation

d = vt + (1/2)at^2 ; where v is initial velocity, t is time, and a is your acceleration.

Once you break the acceleration into it's x and y components, you should be able to get both the x and y distances with the above formula.

Also one thing to note is that the acceleration in the x direction doesn't get effected by gravity, and the acceleration in the y direction is the difference between your original acceleration and gravity. (i.e initial velocity - gravity)
 
  • #3
As a scientist, my response to this content would be to first clarify some important information. Is the rocket being launched from a stationary position or is it already in motion? Is there any air resistance or other external forces acting on the rocket?

Assuming the rocket is being launched from a stationary position and there is no air resistance, we can use the equations provided to find the location of the rocket after 11.2 seconds.

First, we need to find the initial velocity of the rocket in the x and y directions. We can do this by using the given acceleration and the angle of 75 degrees. The initial velocity in the x direction (vix) is equal to the initial velocity (vi) multiplied by the cosine of 75 degrees. Similarly, the initial velocity in the y direction (viy) is equal to the initial velocity (vi) multiplied by the sine of 75 degrees.

Next, we can use the equation a=(vf - vi)/t to find the final velocity (vf) in the x direction. We know the acceleration (a), the initial velocity (vix), and the time (11.2 seconds), so we can solve for vf. Similarly, we can use the equation (vf + vi)/2 = (xf - xi)/t to find the displacement (xf) in the x direction. We know the final velocity (vf), the initial velocity (vix), and the time (11.2 seconds), so we can solve for xf.

To account for gravity, we need to use the same process in the y direction. We can use the initial velocity in the y direction (viy), the acceleration due to gravity (9.8 m/s^2), and the time (11.2 seconds) to find the final velocity (vf) and displacement (yf) in the y direction.

Once we have both the x and y components, we can use the Pythagorean theorem to find the total displacement (d) of the rocket. This will give us the distance from the point of origin after 11.2 seconds.

In summary, to solve for the rocket's location after 11.2 seconds, we need to find the initial velocities in the x and y directions, use the equations for acceleration, velocity, and displacement to find the final values, and then use the Pythagorean theorem to find the total displacement.
 

FAQ: Solving Rocket Launch at 75 Degrees After 11.2s

How do you determine the necessary force to launch a rocket at a 75 degree angle after 11.2 seconds?

To determine the necessary force, we use the formula F=ma, where F is the force, m is the mass of the rocket, and a is the acceleration. We can also use the formula F=mv/t, where F is the force, m is the mass of the rocket, v is the velocity, and t is the time. By plugging in the given values of the angle, time, and mass, we can solve for the necessary force.

What factors affect the trajectory of a rocket launched at a 75 degree angle after 11.2 seconds?

The factors that affect the trajectory of a rocket include the initial force of the launch, the mass of the rocket, the angle of launch, air resistance, and gravity. These factors can all impact the acceleration and velocity of the rocket, which ultimately determine its trajectory.

How does air resistance affect the launch of a rocket at a 75 degree angle after 11.2 seconds?

Air resistance, also known as drag, slows down the rocket as it travels through the air. This means that the rocket will experience less acceleration and velocity, which can affect its trajectory. To account for air resistance, we can use the formula F=kv^2, where F is the force of air resistance, k is a constant, and v is the velocity of the rocket.

How does the mass of the rocket affect its launch at a 75 degree angle after 11.2 seconds?

The mass of the rocket directly affects the force needed to launch it at a certain angle and time. The greater the mass, the greater the force needed to overcome its inertia and accelerate it. Additionally, a heavier rocket may also experience more air resistance, which can affect its trajectory.

How do you account for the effects of gravity on a rocket launched at a 75 degree angle after 11.2 seconds?

Gravity plays a significant role in the trajectory of a rocket. The force of gravity pulls the rocket towards the ground, affecting its acceleration and velocity. To account for this, we can use the formula F=mg, where F is the force of gravity, m is the mass of the rocket, and g is the acceleration due to gravity. This force must be overcome by the initial force of the launch in order for the rocket to achieve its desired trajectory.

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