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Advanced Components for Thermal Control of a Mercury Orbiting Spacecraft EADS SPACE Transportation GmbH

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Antonenko, J., author.
Conference Name:
International Conference On Environmental Systems (2004-07-19 : Colorado Springs, Colorado, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 2004
Summary:
The European Space Agency ESA is preparing a mission to planet Mercury called BepiColombo in cooperation with ISAS, the Japanese space agency. Advanced thermal control materials and components are under development to allow the performance of the mission.The present paper gives an overview of the BepiColombo thermal control design and give emphasis to the continued effort in the development of a Solar Reflector Coating (SRC), an Optical Solar Reflector (OSR) and an Infra-Red Rejection Device (IRRD). Key issue in the development and validation of the components and related technologies is the long-term stability under the high temperature and high intensity radiation environment in the vicinity of Mercury. Therefore thermal and radiation endurance testing plays a major role. Candidate materials have been selected and the component design been defined. Development tests will establish mechanical, thermal and optical properties for the initial and end of life conditions
Notes:
Vendor supplied data
Publisher Number:
2004-01-2520
Access Restriction:
Restricted for use by site license

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