Question: 8 . In the patched conic approximation for interplanetary transfers, what is the hyperbolic excess velocity ( only ) of a spacecraft leaving Mars to

8. In the patched conic approximation for interplanetary transfers, what is the hyperbolic excess velocity (only) of a spacecraft leaving Mars to return to Earth.
Given: Altitude at Mars is 1000 km, Return Parking Orbit (Earth) will be an Altitude of 1000 km .
8 . In the patched conic approximation for

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