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Thermal Design and Test of ROSETTA Platform Louvres
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Technical Paper
2000-01-2276
ISSN: 0148-7191, e-ISSN: 2688-3627
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Language:
English
Abstract
The design and development of the louvre for the ROSETTA spacecraft in the scope of its thermal qualification process are presented. In the first section the design and its development are described. The analytical prediction considering effective emittance and absorbtance of this design are presented in the following section. Tests at unit as well as spacecraft level have been conducted in order to verify the thermal design.
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Citation
Härtel, K., Morgenroth, L., Reichenberger, K., Domingo, M. et al., "Thermal Design and Test of ROSETTA Platform LouvresAlso In
References
- The Red Book - Thermal Control Materials and Films Sheldahl Technical Materials,1150 Sheldahl Road, Northfield, MN 5057.
- Spacecraft Thermal Control Design Data ESA/ESTEC Thermal Control & Life Support Division, Noordwijk, The Netherlands.
- Data for Selection of Space Materials ESA/ESTEC Product Assurance & Safety Department, Noordwijk, The Netherlands.