Design modifications for increasing the BOM and EOM power output and reducing the size and mass of RTG for the Pluto mission
Author:
Affiliation:
1. Fairchild Space and Defense Corp., Germantown, MD
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1994-4129
Reference3 articles.
1. Effect of fuel and design options on RTG performance versus PFF power demand
2. Design, Analysis, and Optimization of RTG for Solar Polar Mission
3. RTGs Options for Pluto Fast Flyby Mission
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