Projectile Motion of a Secondary Rocket in a Vertical Launch

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SUMMARY

The discussion focuses on the physics of a secondary rocket launched from a primary rocket traveling upward at 8.50 m/s. The secondary rocket is launched at a speed of 12 m/s at an angle of 53 degrees. The calculations for the horizontal and vertical components of the secondary rocket's velocity relative to both the astronaut and Mission Control are provided, confirming the correct application of the equations of motion. The vertical component of the secondary rocket's velocity relative to Mission Control is calculated to be 18.0836 m/s, while the horizontal component remains at 7.2217 m/s.

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Homework Statement



When it is 145 m above the ground, a rocket traveling vertically upward at a constant 8.50 m/s relative to the ground launches a secondary rocket at a speed of 12 m/s at an angle of 53 degrees above the horizontal, both quantities being measured by an astronaut sitting in the rocket. Air resistance is too small to worry about.

(a) Just as the secondary rocket is launched, what are the horizontal and vertical components of its velocity relative to (i) the astronaut sitting in the rocket and (ii) Mission Control on the ground?

(b) Find the initial speed and launch angle of the secondary rocket as measured by mission control.

(c) What maximum height above the ground does the secondary rocket reach?



Homework Equations



Vy=Vosin(θ)
Vx=Vocos(θ)

Vr2/e=Vr2/r1+Vr1/e

Vr2/e= velocity of rocket 2 relative to earth
Vr2/r1= velocity of rocket 2 relative to rocket 1
Vr1/e= velocity of rocket 1 relative to earth

The Attempt at a Solution


A)
i:
Vr2/r1-x= 12m/s*cos(53)=7.2217 m/s
Vr2/r1-y= 12m/s*sin(53)=9.5836 m/s

Vr2/e=vr2/r1 + vr1/e

ii: Vr2/e-y=vr2/r1-y + vr1/e-y
Vr2/3-y= 9.5836 m/s + 8.50m/s=18.0836m/s

Vr2/e-x=vr2/r1-x + vr1/e-x
vr2/e-x= 7.2217m/s + 0=7.2217m/s

Do I have part a right so far? thanks!
 
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Toranc3 said:
Do I have part a right so far? thanks!
Looks good to me!
 
Doc Al said:
Looks good to me!

Thank you Doctor!
 

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