A rocket is fired vertically and tracked by the radar R as shown. At a particular angular position with angle of elevation(theta) from radar = 60., measured parameters are r=9 km, dr/dt = 10m/s and d(theta)/dt = 0.002 rad/s. The velocity of rocket at this position is:
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This question is very very simple. I'll use "@" instead of "theta".
Now, y = rSin@ dy/dt = dr/dt.Sin@ + (rCos@)d@/dt = Velocity of rocket
Sunbstituting the given values, we have
velocity of rocket = (10)Sin60 + (9000)(Cos60)(0.002) = 17.7 m/s A better solution is welcomed