Thermal Design and Test of ROSETTA Platform Louvres

Thermal Design and Test of ROSETTA Platform Louvres

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 present...

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Veröffentlicht in:SAE transactions 2000-01, Vol.109, p.394-404
Hauptverfasser: Härtel, K., Morgenroth, L., Reichenberger, K., Domingo, M., Pérez, F.J., Stramaccioni, D.
Format: Artikel
Sprache:eng
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Zusammenfassung: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.
ISSN:0096-736X
2577-1531