HUYGENS Probe: Thermal Design, Test, Flight Comparison, and Descent Prediction

981644

07/13/1998

Event
International Conference On Environmental Systems
Authors Abstract
Content
A study of the first in-orbit temperatures of Huygens shows that the probe will very likely survive thermally all vacuum cruise and coast phases. Calculated heat fluxes, mass flows of Titan's atmosphere into and out of the probe and temperatures give confidence also for the mission phase proper in 2004 i.e. the 2.5 h descent into Titan's -2OO°C atmosphere.
Basotect foam bags insulate the probe from this atmosphere. These bags and their fixation had drastically to be modified between Titan test on STPM (May 95) and on FM (June 96). The mission phases, thermal requirements, thermal design, tests with the probe, special tests for the foam bag development and their modification are presented.
Meta TagsDetails
DOI
https://doi.org/10.4271/981644
Pages
12
Citation
Cluzet, G., Doenecke, J., Vollmer, K., and Patti, B., "HUYGENS Probe: Thermal Design, Test, Flight Comparison, and Descent Prediction," SAE Technical Paper 981644, 1998, https://doi.org/10.4271/981644.
Additional Details
Publisher
Published
Jul 13, 1998
Product Code
981644
Content Type
Technical Paper
Language
English