Maximum altitude of a rocket launch

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Homework Help Overview

The problem involves a rocket launched at an angle of 53 degrees with an initial speed of 100 m/s and an acceleration of 30 m/s² for 3 seconds before its engines fail. The goal is to determine the maximum altitude reached by the rocket after it transitions to free fall.

Discussion Character

  • Exploratory, Assumption checking, Problem interpretation

Approaches and Questions Raised

  • Participants discuss the rocket's position and speed at the moment the engines fail, with calculations for distance and velocity being shared. Questions arise about how to express time to reach maximum altitude and the relevance of time in the context of the problem.

Discussion Status

Some participants have provided guidance on using kinematic equations to find the vertical component of velocity and how to approach the calculation of maximum altitude. There is an ongoing exploration of the relationship between time, velocity, and displacement after the engines fail, with no explicit consensus reached.

Contextual Notes

Participants note the need to consider both the distance traveled while the engines were active and the distance during free fall to determine the total maximum altitude. There is also mention of gravitational acceleration affecting the rocket after engine failure.

imatreyu
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Homework Statement



A rocket is launched at an angle of 53 degrees above the horizontal with an intial speed of 100 m/s. It moves along its initial line of motion with an accel. of 30 m/s^2 for 3 s. At this time its engines fail and the rocket proceeds to move as a free body. Find the maximum altitude reached by the rocket.

Homework Equations


Just the four basic kinematics equations. . ?

The Attempt at a Solution


I did:

where is the rocket when its engines fail?
d= vit + (1/2)at^2
= 100 sin 53 (3) + (1/2)(30)(3^2)
= 374.59 m

what is the rocket's speed after the engines fail?
vf= vi + at
=100 + 30 (3)
=190 m/s

So I feel like from here I should just be able to plug into vf^2= vi^2 + 2ad and find "d," using vi= 190 m/s and vf= 0. . . .But that's not the case. Why can't I do that? And where can I go from here? I have a feeling I need to find some way to express time to reach the maximum altitude, but I have no idea how I can express that.

~Thank you in advance!
 
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At what angle is the rocket traveling when its engines cut?
 
The rocket is traveling at 53 degrees above the horizontal when its engine is cut.
 
So what are the components of its velocity at the time that the engine cuts? How can you use the vertical component to calculate the time it takes to reach maximum altitude? How can that time be used to find the vertical displacement of the rocket after the engines cut?
 
1. Components of initial velocity: vix= 100cos53, viy= 100sin53
2. I honestly have no idea. :( I don't know what equation to create. . how to express time. . .
3. . . .
 
When the engine fails, it's velocity is 190 m/s at 53 degrees from horizontal.

Then in the vertical direction, you can use the equation Vf = Vi + at, where Vf = 0, Vi = 190sin53 m/s , a = -9.8 m/s^2, and isolate t.

Go from there.
 
Oh. . .
So viy= 190sin53, vfy= 0?

I think I can see how I could use that to find time to fall in one of the kinematics equations, but I don't see how I could express time to reach maximum altitude.
 
Remeber that after engines fails, the only acceleration on the rocket is gravity.
 
Is time even relevant, then?

Or can I just do this:

vf^2 = vi^2 -2(9.8)d
vf= 0 (because at apogee velocity is s 0, and apogee would be the maximum altitude)
viy= 190sin53

and then solve for d?
 
  • #10
Yes, but breaking it down helps to visualize it, no? And you asked for a way to express time, so I showed you.

Plus, it asks for max altitude, this 'd' is only from free fall. We have to add the 'd' from rocket thrust upwards.

Hope I helped.
 
Last edited:
  • #11
Ohh. . . .Haha the time thing was a result of Yahoo answers confusion.

Oh, and then I add the initial distance.
Aha! I get it!
THANK YOU SO MUCH!
 

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