- Joined
- 16 December 2010
- Messages
- 3,746
- Reaction score
- 4,072
Proposed design for a Multi-Mission bus using ion engines for propulsion. Suggested missions included an untargeted asteroid belt flyby, a targeted asteroid belt flyby, a Jupiter flyby (With or without use of gravity assist to reach an out-of-ecliptic orbit following the flyby.) and a out-of-ecliptic mission using the ion engines to slowly change the spacecraft inclination relative to the ecliptic over several orbits.
The planned launch vehicles would have been the Atlas-Centaur (Asteroid belt missions) or the Titan IIIc (Jupiter/Out-of-Ecliptic).
Study of a Solar Electric Multi-Mission Spacecraft
https://app.box.com/s/ch93bcikj6pj49nkfika1ody2msmmr4k
The planned launch vehicles would have been the Atlas-Centaur (Asteroid belt missions) or the Titan IIIc (Jupiter/Out-of-Ecliptic).
Study of a Solar Electric Multi-Mission Spacecraft
https://app.box.com/s/ch93bcikj6pj49nkfika1ody2msmmr4k
Attachments
-
Solar_Electric_Multi-Mission_Spacecraft_01.png514 KB · Views: 367
-
Solar_Electric_Multi-Mission_Spacecraft_02.png165.2 KB · Views: 325
-
Solar_Electric_Multi-Mission_Spacecraft_03.png284.1 KB · Views: 295
-
Solar_Electric_Multi-Mission_Spacecraft_04.png380.3 KB · Views: 268
-
Solar_Electric_Multi-Mission_Spacecraft_05.png276 KB · Views: 249
-
Solar_Electric_Multi-Mission_Spacecraft_06.png312.9 KB · Views: 43