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 = 2×100 where E is the energy, in r Joules, and r is the new radius, in kilometers. a) Determine x-intercept(s) if it exists. b) Determine y-intercept(s) if it exists. c) Determine the equations of the horizontal asymptote if it exists. d) Determine the equations of the vertical asymptote(s) if it exists.

Algebra & Trigonometry with Analytic Geometry
13th Edition
ISBN:9781133382119
Author:Swokowski
Publisher:Swokowski
Chapter11: Topics From Analytic Geometry
Section11.3: Hyperbolas
Problem 35E
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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:
where E is the energy, in
r
Joules, and r is the new radius, in kilometers.
a) Determine x-intercept(s) if it exists.
b) Determine y-intercept(s) if it exists.
c) Determine the equations of the horizontal asymptote if it exists.
d) Determine the equations of the vertical asymptote(s) if it exists.
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: where E is the energy, in r Joules, and r is the new radius, in kilometers. a) Determine x-intercept(s) if it exists. b) Determine y-intercept(s) if it exists. c) Determine the equations of the horizontal asymptote if it exists. d) Determine the equations of the vertical asymptote(s) if it exists.
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