python 3

Escape Velocity "The energy E necessary to bring a unit of mass into a circular satellite orbit neglecting drag, consists of kinetic and potential energy, namely 2 points where g 9.8 is the acceleration due to gravity and us is the satellite velocity RO RFr where Ro is the radius of the Earth and h is the height above the Earth at which the satellite orbits. What is the energy E necessary to put a satellite into orbit at h 10 x 10m, in units of J? Work in Sl 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._ Starter code (click to view) Answer1import sympy Escape Velocity "The energy E necessary to bring a unit of mass into a circular satellite orbit neglecting drag, consists of kinetic and potential energy, namely 2 points where g 9.8 is the acceleration due to gravity and us is the satellite velocity RO RFr where Ro is the radius of the Earth and h is the height above the Earth at which the satellite orbits. What is the energy E necessary to put a satellite into orbit at h 10 x 10m, in units of J? Work in Sl 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._ Starter code (click to view) Answer1import sympy