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IUS application to NASA planetary missionsThe 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.
Document ID
19880028705
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hanford, Denton
(Boeing Aerospace Co. Seattle, WA, United States)
Saucier, Sidney
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 13, 2013
Publication Date
October 1, 1987
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
IAF PAPER 87-195
Accession Number
88A15932
Distribution Limits
Public
Copyright
Other

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