A rocket, rising vertically, is tracked by a radar station that is on the ground 5 miles from the launch pad. At what rate is the elevation angle changing when the rocket is 3000 feet up and rising vertically at 500 ft/sec?
First: C^2=B^2+A^2, A=the path of the rocket=3000'. B=the distance from the lanchpad of the radar station=5 miles or 26400' so, C=26569.9'
Now, I take the derivaitive of both sides:
2C dC/dt=2B dB/dt + 2A dA/dt
2(26569.9) dC/dt=2(26400) dB/dt + 2(3000) dA/dt
53139.8 dC/dt=52800 dB/dt + 6000 dA/dt
53139.8 dC/dt= 52800(0)(no rate change for B) + 6000(500)
dC/dt= 3000000/53139.8
dC/dt=56.46
sin(dA/dt)/(dC/dt)=sin(500/56.46) =.537 Rad
What am I doing wrong?????
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First: C^2=B^2+A^2, A=the path of the rocket=3000'. B=the distance from the lanchpad of the radar station=5 miles or 26400' so, C=26569.9'
Now, I take the derivaitive of both sides:
2C dC/dt=2B dB/dt + 2A dA/dt
2(26569.9) dC/dt=2(26400) dB/dt + 2(3000) dA/dt
53139.8 dC/dt=52800 dB/dt + 6000 dA/dt
53139.8 dC/dt= 52800(0)(no rate change for B) + 6000(500)
dC/dt= 3000000/53139.8
dC/dt=56.46
sin(dA/dt)/(dC/dt)=sin(500/56.46) =.537 Rad
What am I doing wrong?????
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