Maximum altitude of a rocket in 2D motion and free body motion

AI Thread Summary
The discussion focuses on calculating the maximum altitude of a rocket launched at a 53-degree angle with an initial speed of 75 m/s and an acceleration of 25 m/s² for 25 seconds before its engines fail. The initial calculations suggest a maximum vertical displacement of 7750 meters, derived from the displacement equation using the vertical components of velocity and acceleration. The user expresses confusion over the results when applying the same method to a different problem, leading to inconsistent answers. Clarification is sought regarding the rocket's velocity at the point of fuel depletion, emphasizing the need to correctly account for the acceleration in the calculations. The conversation highlights the importance of accurately interpreting the motion dynamics in projectile problems.
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Homework Statement



A rocket is launched at an angle of 53 above the horizontal with an initial speed of 75 m/s. It moves for 25s along it's initial line of motion with an overall acceleration of 25 m/22. At this time its engines fail and the rocket proceeds to move as a freebody.

a) What is the rocket's maximum altitude?

Homework Equations



displacement = V1time + (1/2)a(time)2
V2 = V1 + 2adisplacement

The Attempt at a Solution



I've googled this question after attempting it, and have seen several different methods from my own.

For part a, I'm interpreting it as the maximum vertical displacement. I set up a vector diagram, where the angle between the average velocity vector and horizontal velocity vector is 53. I use sin ratio to solve for the opposite, which is sinTHETA x hyp. This gives me 60m/s. I do the same process to find the vertical acceleration, which is 20.0 m/s2. I plug them into the displacement equation, solve to get 7750m.

Now for the free body motion. Velocity will equal 0 when it gets to it's top. I use the second equation to rearrange for displacement. V2 is 0, V1 is -602, acceleration is -9.81. Essentially, displacement is a negative value. Meaning the max. altitude is still 7750m.

Makes sense to me, but I applied the same approach to a different question (identical) with diff. values. The answer was way off. (I did this to see if my approach was right).

What am I doing wrong?
 
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What will be the rocket's velocity when it runs out of fuel?

V1 is -602
V1 isn't 60m/s because the rocket has been accelerating.
 
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