p14 059

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59. The total energy is given by E =

−GMm/2a, where M is the mass of the central attracting body (the

Sun, for example), m is the mass of the object (a planet, for example), and a is the semimajor axis of
the orbit. If the object is a distance r from the central body the potential energy is U =

−GMm/r.

We write

1
2

mv

2

for the kinetic energy. Then, E = K + U becomes

−GMm/2a =

1
2

mv

2

− GMm/r. We

solve for v

2

. The result is

v

2

= GM



2

r

1

a



.


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