disvusneM fumabong & I sidnT 5) What is the delta-y and propellant required for a spacecraft to achieve planetary orbit around Mars (V. = 5 km/sec) if the propulsion system delivers 310 seconds of iM specific impulse and the final mass of the spacecraft is 1500 kg. The parking orbit has a periapsis radius of 10,000 km and an eccentricity of 0.35. Assume you capture 20 into orbit at periapsis. (25 pts.) OTV er maleve nofelugong buspil sbom laub ofT