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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 = 30°, the tracking data give r = 25(104) ft, i = 4000 ft/sec, and é = 0.80 degisec. 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 u of the rocket and the values of F and 6.

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 = 30°, the tracking data give r = 25(104) ft, i = 4000 ft/sec, and é = 0.80 degisec. 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 u of the rocket and the values of F and 6.

College Physics
College Physics
11th Edition
ISBN:9781305952300
Author:Raymond A. Serway, Chris Vuille
Publisher:Raymond A. Serway, Chris Vuille
Chapter1: Units, Trigonometry. And Vectors
Section: Chapter Questions
Problem 1CQ: Estimate the order of magnitude of the length, in meters, of each of the following; (a) a mouse, (b)...
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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 0 = 30°, the tracking data give r = 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 u of the rocket and the values of F and 6. 25(10) ft, i = 4000 ft/sec, and é 0.80 deg/sec.
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 0 = 30°, the tracking data give r = 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 u of the rocket and the values of F and 6. 25(10) ft, i = 4000 ft/sec, and é 0.80 deg/sec.
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