534 Solutions Manual
Problem 3.83
A satellite orbits the Earth as shown. Model the satellite as a
particle, and assume that the center of the Earth can be chosen as
the origin of an inertial frame of reference.
The minimum and maximum distances from the center of
the Earth are
RPD4:5 ⇥107
m and
RAD6:163⇥107
m, re-
spectively, where the subscripts
P
and
A
stand for perigee (the
point on the orbit closest to Earth) and apogee (the point on
the orbit farthest from Earth), respectively. If the satellite’s speed
at Pis vPD3:2⇥103m=s, determine the satellite’s speed at A.
Solution
of McGraw-Hill, and must be surrendered upon request of McGraw-Hill. Any duplication or distribution, either in print or electronic form, without the
permission of McGraw-Hill, is prohibited.