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 E = 2×10" where E is the energy, in Joules, and r is the new radius, in kilometers. a) How much energy must be given to the satellite ifr= 12 000 km? b) Calculate the new radius of the satellite if 10º Joules of energy are added to it. c) How much energy must be given to the satellite in order for it to escape Earth’s gravity completely (make its orbit's radius infinitely large)?

Advanced Engineering Mathematics
10th Edition
ISBN:9780470458365
Author:Erwin Kreyszig
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Chapter2: Second-order Linear Odes
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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 E = 2 ×1010
where E is the energy, in
Joules, and r is the new radius, in kilometers.
a) How much energy must be given to the satellite if r= 12 000 km?
b) Calculate the new radius of the satellite if 100 Joules of energy are added to it.
c) How much energy must be given to the satellite in order for it to escape Earth's gravity completely
(make its orbit's radius infinitely large)?
Transcribed Image Text: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 E = 2 ×1010 where E is the energy, in Joules, and r is the new radius, in kilometers. a) How much energy must be given to the satellite if r= 12 000 km? b) Calculate the new radius of the satellite if 100 Joules of energy are added to it. c) How much energy must be given to the satellite in order for it to escape Earth's gravity completely (make its orbit's radius infinitely large)?
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