PEARSON ETEXT ENGINEERING MECH & STATS
PEARSON ETEXT ENGINEERING MECH & STATS
15th Edition
ISBN: 9780137514724
Author: HIBBELER
Publisher: PEARSON
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The rocket is travelling in a free-flight elliptical orbit about the earth such that eccentiricty is e and it's perigee is a distance d as shown. Determine it's speed when it is at point B. Also determine the sudden decrease in speed the rocket must experience at A in order to travel in a circular orbit.
The 245-kg glider Bis being towed by airplane A, which is flying horizontally with a constant speed of v = 183 km/h. The tow cable has a length r = 59 m and may be assumed to form a straight line. The glider is gaining altitude and when e reaches 14°, the angle is increasing at the constant rate 0 = 8 deg/s. At the same time the tension in the tow cable is 2370 N for this position. Calculate the aerodynamic lift L and drag D acting on the glider. Assume o = 10°. D B A
1. The satellite is moving in an elliptical orbit with an eccentricity e = 0.25. Determine its speed when it is at its maximum distance A and minimum distance B from the earth. 2 Mm B
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