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.
Thermal Design and Test of ROSETTA Platform Louvres*
Sae Technical Papers
International Conference On Environmental Systems ; 2000
10.07.2000
Aufsatz (Konferenz)
Englisch
Thermal Design and Test of ROSETTA Platform Louvres
British Library Conference Proceedings | 2000
|Mechanical Design and Test of Rosetta Platform Louvres
British Library Conference Proceedings | 2003
|Thermal Louvres von Magna Steyr Space Technology
Kraftfahrwesen | 2004
|Wind-tunnel tests of air intake louvres
Engineering Index Backfile | 1937
|