Suppose a probe satellite of mass m is released with some initial velocity Vo out in space, far away from some mystery planet of mass M The satellite is observed to speed up, whip around the mystery planet, and continue to off to infinity at angle of 90° relative to it's incoming path. What is the eccentricity of the trajectory?

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Chapter7: Gravitation
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Suppose a probe satellite of mass m is released with some initial velocity Vo out in space, far away from some mystery planet of mass M The
satellite is observed to speed up, whip around the mystery planet, and continue to off to infinity at angle of 90° relative to it's incoming path. What is the
eccentricity of the trajectory?
O e = 2
Oe=
-3/2
O e = v2
3/2
e =
Transcribed Image Text:Suppose a probe satellite of mass m is released with some initial velocity Vo out in space, far away from some mystery planet of mass M The satellite is observed to speed up, whip around the mystery planet, and continue to off to infinity at angle of 90° relative to it's incoming path. What is the eccentricity of the trajectory? O e = 2 Oe= -3/2 O e = v2 3/2 e =
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