6:36 1A space probe is to be placed in a circular orbit of radius 4000 km about the planet Mars. As the probe reaches A the point of itsoriginal trajectory closest to Mars, it is inserted into a first elliptic transfer orbit by reducing its speed. This orbit brings it to Point 8 witha much reduced velocity. There the probe is inserted into a second transfer orbit by further reducing its speed. Knowing that the massof Mars is 0.1074 times the mass of the earth, that rA 9004 km and rg- 180 004 km, and that the probe approaches A on a parabolictrajectory, determine the time needed for the space probe to travel from A to Bon its first transfer orbit.Apph traretrySeend trader ctaFinttranferThe time needed for the space probe to travel from A to Bon its first transfer orbit is Oh

Given: Earth radius, Re=6373 km=6.373×106 m GMe=gR2GMe=9.816.373×1062GMe=398.43×1012 m3/s2 Mars…

Answered: A space probe is to be placed in a…

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