The considerations involved in the selection of a new upper stage to launch three planetary missions following the decision to cancel the use of Centaur are discussed, and the methods by which the selected IUS will fly these missions are described. It is shown that the IUS is capable of accomplishing all three misssions (Magellan, Galileo, and Ulysses) with some compromises in mission transit time. Relatively minor modifications to the IUS, airborne support equipment, and software are required. The first of the three missions is to be accomplished two and a half years from go-ahead by the use of existing IUS flight hardware.
IUS application to NASA planetary missions
1987-10-01
Conference paper
No indication
English
Battery requirements for future NASA planetary missions
Tema Archive | 1982
|A Small Fission Power System For NASA Planetary Science Missions
Online Contents | 2011
|