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Characterising the Thermal Performance of the European Comet Chaser ROSETTA
Technical Paper
2003-01-2464
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
This paper describes the processes and evolution of the design and verification of the thermal control subsystem of the Rosetta spacecraft. In particular, it describes the testing, both at component-level and spacecraft-level, that was necessary and the subsequent correlation activities that were required to understand the thermal behaviour of the spacecraft and thus develop a thermal model that portrayed this correctly.
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Citation
Tuttle, S., Kerner, R., and Stramaccioni, D., "Characterising the Thermal Performance of the European Comet Chaser ROSETTA," SAE Technical Paper 2003-01-2464, 2003, https://doi.org/10.4271/2003-01-2464.Also In
References
- Price, S.G. Spilling, D.A.V. Tuttle, S.L. ROSETTA Spacecraft initial thermal design ICES Denver, Colorado, USA August 1999
- ESA Bulletin no. 112 November 2002
- Hartel K. Morgenroth L. Thermal Design and Test of ROSETTA Platform Louvres ICES Toulouse, France July 2000