Mission Design for the Exploration of Neptune and Triton
Abstract
This paper discusses some enabling technologies for an ESA-led Neptune orbiter mission with multiple Triton flybys, with emphasis on the trajectory design. The spacecraft dry mass is comparable to that of the planetary orbiters to Jupiter and Saturn.
- Publication:
-
Workshop on the Study of the Ice Giant Planets
- Pub Date:
- July 2014
- Bibcode:
- 2014LPICo1798.2012C