Halsell, C. A.; Bowes, A.; Lyons, D. T.; Johnston, M. D.; Lock, R. E.; Xaypraseuth, P.; Bhaskaran, S.; Highsmith, D. E.; Jab, M. K.
(2002-02-09)
This paper describes the analysis and design evolution of the Mars Reconnaissance Orbiter trajectory from launch to end-of-mission. The mission uses a combination of propulsive maneuvers and aerobraking techniques to deliver ...