Advanced physics... Determine the Delta-V in km/s for the described maneuver by the MRO spacecraft.

7.32 In March 2006, the Mars Reconnaissance Orbiter (MRO) spacecraft approached Mars on a hyperbolic trajectory with asymptotic approach speed v50 = 2.9572 [cm/s. Mars orbit insertion (MOI) occurred at periapsis by ring six rocket engines. The MOI burn produced an elliptical orbit with periapsis and apoapsis altitudes of 426 and 44,500 km, respectively. Determine the Av for this impulsive maneuver [note that Mars'radius is RM 2 3,396 km and its gravitational parameter is m = 4.2323004) knit/st]