Characterising the Thermal Performance of the European Comet Chaser ROSETTA 2003-01-2464
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.
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. Download Citation
Author(s):
S. L. Tuttle, R. Kerner, D. Stramaccioni
Pages: 15
Event:
International Conference On Environmental Systems
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Spacecraft
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