Problem 4 (10 pts.): Two elliptical orbits share the same central body and apsidal line as shown in below figure. Point A lies at the apogee of orbit 1. Point B lies at the apogee of orbit 2. Perform a Hohmann transfer from point A to point B. All numbers have been non-dimensionalzed such that μ 1. The apogee and perigee of orbit 1 and 2 are given by = = 10 and Respectively. What is the total Av for the maneuver? 11p₁ = 4 √√₁2 = 8 (p2 = 3 Point B

Fig: 1