The amount of energy needed to increase the radius of orbit of a 500-kg satellite from its original orbit r -10 000 of radius 10 000 km can be modelled by the function =. where E is the energy, in Joules, and r is the new radius, in kilometers. a) Determine the average rate of change between r= 10 000 km and r = 15 000 km. b) Determine the instantaneous rate of change at r = 15 000 km. c) What is the difference between an average rate of change and an instantaneous rate of change?
The amount of energy needed to increase the radius of orbit of a 500-kg satellite from its original orbit r -10 000 of radius 10 000 km can be modelled by the function =. where E is the energy, in Joules, and r is the new radius, in kilometers. a) Determine the average rate of change between r= 10 000 km and r = 15 000 km. b) Determine the instantaneous rate of change at r = 15 000 km. c) What is the difference between an average rate of change and an instantaneous rate of change?
Advanced Engineering Mathematics
10th Edition
ISBN:9780470458365
Author:Erwin Kreyszig
Publisher:Erwin Kreyszig
Chapter2: Second-order Linear Odes
Section: Chapter Questions
Problem 1RQ
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