Projectile Motion of a fired rocket

AI Thread Summary
The discussion revolves around calculating the maximum altitude and horizontal distance of a rocket launched at an angle of 53.1 degrees with constant acceleration equal to g. The maximum height is derived from the combined height during powered flight and projectile motion, leading to the equation H = 1/2(gSin[53.1])T^2 + u^2Sin^2[53.1]/2g. The initial velocity u is expressed in terms of T, resulting in the expected answer of (18/25)gT^2 for maximum height. The user expresses uncertainty regarding the calculation of horizontal distance, indicating a need for further assistance. The discussion emphasizes the application of kinematic equations in projectile motion analysis.
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Homework Statement


(Q) A rocket is initially at rest on the ground. When its engines fire, the rocket flies off in a straight line at an angle 53.1 degrees above the horizontal with a constant acceleration of magnitude g. The engines stop at a time T after launch, after which the rocket is in projectile motion. You can ignore air resistance and that g is independent of altitude.

Find the maximum altitude reached by the rocket as well as the horizontal distance from the launch point to the point where the rocket hits the ground.



Homework Equations


s=1/2at^2, Hmax for projectile = u^2Sin^2[x]/2g, Time of flight of projectile = 2uSin[x]/g. Also, by equation of motion, u^2 = 2as


The Attempt at a Solution



For the Maximum height, it will be the height traveled in time T plus the maximum height reached when in projectile motion.

Therefore, H = 1/2(gSin[53.1])T^2 + u^2Sin^2[53.1]/2g
But u^2 = 2(gSin[53.1])(1/2(gSin[53.1])T^2).

However, the answer is supposed to be (18/25)gT^2.

As for the horizontal distance, I am completely clueless.

Please help me!

Thank-you very much for your time and effort.
 
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Use sin(53.1 degrees) = 0.8 and cos(53.1 degrees) = 0.6.
 
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