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Heat Transfer in Porous Insulations DASA/ERNO Raumfahrttechnik GmbH

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Ebeling, W. -D, author.
Conference Name:
International Conference On Environmental Systems (1994-06-20 : Friedrichshafen, Germany)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1994
Summary:
When gas conductance/natural convection plays a major role as heat transfer path, microporous insulations reveal distinct advantages compared to Multi-Layer Insulations (MLI). For re-entry vehicles as e. g. HERMES or capsules silica and ceramic microfiber insulations have been investigated by DASA/ERNO in a temperature range up to 650 °C or, respectively, up to 1200 °C. In the frame of an ESTEC funded study three types of microporous insulations - microfiber, microsphere and polyimide foam - have been analytically and experimentally investigated as candidates for the internal insulation of a MARS-lander in a carbon-dioxide atmosphere for temperatures ranging from - 110 °C to 50 °C. This paper compares the test results with analytical heat transfer calculations and describes methods to improve the thermal insulation performance
Notes:
Vendor supplied data
Publisher Number:
941513
Access Restriction:
Restricted for use by site license

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