Design and Modeling of a Variable Heat Rejection Radiator
Design and Modeling of a Variable Heat Rejection Radiator
- Neue Suche nach: Miller, Jennifer R.
- Neue Suche nach: Birur, Gajanana C.
- Neue Suche nach: Ganapathi, Gani B.
- Neue Suche nach: Sunada, Eric T.
- Neue Suche nach: Berisford, Daniel F.
- Neue Suche nach: Stephan, Ryan
- Neue Suche nach: Miller, Jennifer R.
- Neue Suche nach: Birur, Gajanana C.
- Neue Suche nach: Ganapathi, Gani B.
- Neue Suche nach: Sunada, Eric T.
- Neue Suche nach: Berisford, Daniel F.
- Neue Suche nach: Stephan, Ryan
Variable Heat Rejection Radiator technology needed for future NASA human rated & robotic missions Primary objective is to enable a single loop architecture for human-rated missions (1) Radiators are typically sized for maximum heat load in the warmest continuous environment resulting in a large panel area (2) Large radiator area results in fluid being susceptible to freezing at low load in cold environment and typically results in a two-loop system (3) Dual loop architecture is approximately 18% heavier than single loop architecture (based on Orion thermal control system mass) (4) Single loop architecture requires adaptability to varying environments and heat loads
Dokumentinformationen
Design and Modeling of a Variable Heat Rejection Radiator
2011 Spacecraft Thermal Control Workshop ; 2011 ; El Segundo, CA, United States
2011-03-08
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Englisch
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