Question

Assume you have a rocket in Earth orbit and want to go to Mars. The required change in velocity is AV 9.6 km/s. There are two options forthe propulsion system --- chemical and electric --- each with a different specific impulse. Recall that the relationship between specific impulse andexhaust velocity is:Vex = go Isp9.81 m/s2, calculate the propellant fraction required to achieve the necessary AV for each ofUsing the Ideal Rocket Equation and setting gopropulsion system.Part 1: Cryogenic Chemical PropulsionFirst, consider a cryogenic chemical propulsion system with Isp 450 s. Enter the required propellant fraction as a proportion with at least 2decimal places (i.e., enter 0.25 to represent 25%):please answer this quickly​

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