Aspacecraft approaches jupiter on a hohmann transfer ellipse from the earth. it will fly by jupiter at an altitude of 20,000 km on the sunlit side of the planet. calculate
a. jupiter’s heliocentric velocity
b. the spacecraft’s heliocentric velocity upon arrival at jupiter’s sphere of influence
c. the spacecraft’s hyperbolic excess velocity
d. the eccentricity and turn angle of the hyperbolic flyby trajectory
e. the spacecraft’s heliocentric velocity at the outbound crossing of the sphere of influence. how does it compare to your answer to part b?
f. the angular momentum of the new heliocentric orbit after flyby.