A tracking radar lies in the vertical plane of the path of a rocket which is coasting in unpowered flight above the atmosphere. For the instant when e = 30°, the tracking data give r 25x104 ft, v, = 4000 ft/sec, and w = 0.80 deg/sec. The acceleration of the rocket is due only to gravitational attraction and for its particular altitude is 31.4 ft/sec? vertically down. For these conditions determine the velocity of the rocket v, the acceleration of r a, and angular acceleration a.

Structural Analysis
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Chapter2: Loads On Structures
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A tracking radar lies in the vertical plane of the path of a rocket which is coasting in unpowered flight above the atmosphere. For
the instant when e = 30°, the tracking data giver = 25x104 ft, v, = 4000 ft/sec, and w = 0.80 deg/sec. The acceleration of the
rocket is due only to gravitational attraction and for its particular altitude is 31.4 ft/sec? vertically down. For these conditions
determine the velocity of the rocket v, the acceleration of r a, and angular acceleration a.
+r
+0
Transcribed Image Text:A tracking radar lies in the vertical plane of the path of a rocket which is coasting in unpowered flight above the atmosphere. For the instant when e = 30°, the tracking data giver = 25x104 ft, v, = 4000 ft/sec, and w = 0.80 deg/sec. The acceleration of the rocket is due only to gravitational attraction and for its particular altitude is 31.4 ft/sec? vertically down. For these conditions determine the velocity of the rocket v, the acceleration of r a, and angular acceleration a. +r +0
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