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COMPASS Final Report: Saturn Moons Orbiter Using Radioisotope Electric Propulsion (REP): Flagship Class MissionThe COllaborative Modeling and Parametric Assessment of Space Systems (COMPASS) team was approached by the NASA Glenn Research Center (GRC) In-Space Project to perform a design session to develop Radioisotope Electric Propulsion (REP) Spacecraft Conceptual Designs (with cost, risk, and reliability) for missions of three different classes: New Frontier s Class Centaur Orbiter (with Trojan flyby), Flagship, and Discovery. The designs will allow trading of current and future propulsion systems. The results will directly support technology development decisions. The results of the Flagship mission design are reported in this document
Document ID
20110008243
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Oleson, Steven R.
(NASA Glenn Research Center Cleveland, OH, United States)
McGuire, Melissa L.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
February 1, 2011
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
E-17600
NASA/TM-2011-216972
CD-2007-19
Funding Number(s)
WBS: WBS 346620,02,01,02.03,01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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