In this problem, take Earth's and Mars' solar orbits to be coplanar circles with radii 1 and 1.524 AU,respectively. Mars' radius and gravitational parameter are 3393 km and 4.297×104 km?/s² respectively.A probe arrives at Mars after an Earth-Mars Hohmann transfer.What is the probe's heliocentric speed as it approaches Mars?(km/s)(b).What is the probe's speed, with respect to Mars, as it approaches Mars?(km/s)(c) .The probe is steered so that it performs a hyperbolic approach to Mars with periapsis altitude 200 km. WhatAV, applied collinearly at periapsis, will slow the probe down so that it is captured into circular orbit?(km/s)

Given, Mars' radius = 3393 km Gravitational parameter = 4.297 ×104

Answered: In this problem, take Earth's and Mars'…

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