If we want to propel a portion of the rocket to infinity in

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Suppose the rocket was initially on a circular orbit around Earth with a period of 1.2 days.

(a) What is its orbital speed?

(b) If we want to propel a portion of the rocket to infinity (in the direction tangential to the circular orbit), what's the escape speed from there?

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If we want to propel a portion of the rocket to infinity in : suppose the rocket was initially on a circular orbit around earth with a period of 1.2 days.a what is its orbital

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