Problem 14.117 The time required for a satellite in a
circular earth orbit to complete one revolution increases
as the radius of the orbit increases. If you choose the
radius properly, the satellite will complete one revolu-
tion in 24 hours. If a satellite is placed in such an orbit
directly above the equator and moving from west to east,
it will remain above the same point on the earth as the
earth rotates beneath it. This type of orbit, conceived
by Arthur C. Clarke, is called geosynchronous, and is
used for communication and television broadcast satel-
lites. Determine the radius of a geosynchronous orbit
in km.
Solution: We have
Problem 14.118* You can send a spacecraft from the
earth to the moon in the following way. First, launch
the spacecraft into a circular “parking” orbit of radius
r0around the earth (Fig. a). Then increase its velocity
in the direction tangent to the circular orbit to a value
v0such that it will follow an elliptic orbit whose maxi-
mum radius is equal to the radius rMof the moon’s orbit
around the earth (Fig. b). The radius rM=238,000 mi.
Let r0=4160 mi. What velocity v0is necessary to send
a spacecraft to the moon? (This description is simplified
in that it disregards the effect of the moon’s gravity.)
Parking
orbit
r0r0
v0
rM
Elliptic
orbit
Moon’s
orbit
(a) (b)