A spacecraft arrives at Mars’ sphere of inﬂuence with a heliocentric velocity of 22 km/s and...

A spacecraft arrives at Mars’ sphere of inﬂuence with a heliocentric velocity of 22 km/s and a heliocentric ﬁght-path angle of 10 deg. When the spacecraft reaches the periapsis of its Mars-centric arrival trajectory, at an altitude of 200 km, it performs a ∆V to circularize its trajectory. What is the required ∆V ?

Expert Solution

genius_generous answered 1 year ago

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