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.
Characterising the Thermal Performance of the European Comet Chaser ROSETTA
Sae Technical Papers
International Conference On Environmental Systems ; 2003
2003-07-07
Conference paper
English
Characterising the Thermal Performance of the European Comet Chaser ROSETTA
British Library Conference Proceedings | 2003
|Comet chaser . ESA Rosetta mission to land on comet
Online Contents | 1999
The New Mission of ‘Rosetta’ Comet Chaser and In-Orbit First Temperature Results
SAE Technical Papers | 2004
|The New Mission of Rosetta Comet Chaser and In-Orbit First Temperature Results
British Library Conference Proceedings | 2004
|