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The New Mission of Rosetta Comet Chaser and In-Orbit First Temperature Results European Space Agency, ESTEC, Noordwijk, NL

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Stramaccioni, D., author.
Conference Name:
International Conference On Environmental Systems (2004-07-19 : Colorado Springs, Colorado, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 2004
Summary:
The Rosetta spacecraft was re-targeted to a newly selected comet following a one-year launch delay. The thermal control of the spacecraft has to cope with a large Sun distance range - 0.88 to 5.35 AU - and increasing comet activity combined with operational conditions that span from full payload activity to power saving hibernation mode. The new mission stretches the range of solar flux even further than the original mission and some adaptations to the thermal hardware were required. This paper describes how the new demanding mission scenario influenced the thermal design of the spacecraft and its operations. Then, the thermal behaviour of the spacecraft as revealed by the first in-orbit results is evaluated and compared where possible with the response anticipated by the analyses and by the environmental thermal test programme results. Rosetta was injected into an Earth escape trajectory on March 2th 2004 by an Ariane 5 dedicated launch
Notes:
Vendor supplied data
Publisher Number:
2004-01-2356
Access Restriction:
Restricted for use by site license

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