DONE IN PYTHON

Escape Velocity 2 points "The energy E necessary to bring a unit of mass into a circular satellite orbit neglecting drag, consists of kinetic and potential energy, namely dRg ' where g 9.8 is the acceieration due to gravity and u, is the satellite velocity w, where Ro is the radius of the Earth (5) and Shs is the , where Ro is the radius of the Earth (S$) and Sh$ is the Roth height above the Earth at which the satellite orbits. what is the energy E necessary to put a satellite into orbit at h = 10 106 m, in units of J ? Work in SI to obviate the need for a unit system in this problem. Store your result in a variable energy, which should be a sympy expression. You should also include an intermediate variable us which should also be a sympy expression. Use the symbolic variable R0 instead of R_0 to be consistent with the autograder. This exercise (and the quote) is derived from Sutton & Biblarz,-Rocket Propulsion Elements, p. 120"- Escape Velocity 2 points "The energy E necessary to bring a unit of mass into a circular satellite orbit neglecting drag, consists of kinetic and potential energy, namely dRg ' where g 9.8 is the acceieration due to gravity and u, is the satellite velocity w, where Ro is the radius of the Earth (5) and Shs is the , where Ro is the radius of the Earth (S$) and Sh$ is the Roth height above the Earth at which the satellite orbits. what is the energy E necessary to put a satellite into orbit at h = 10 106 m, in units of J ? Work in SI to obviate the need for a unit system in this problem. Store your result in a variable energy, which should be a sympy expression. You should also include an intermediate variable us which should also be a sympy expression. Use the symbolic variable R0 instead of R_0 to be consistent with the autograder. This exercise (and the quote) is derived from Sutton & Biblarz,-Rocket Propulsion Elements, p. 120