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MIRKA Heat Shield Experiment HEATIN-Theoretical and Experimental Approach to the Surface Protected Ablator

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Reich, G., author.
Conference Name:
International Conference On Environmental Systems (1996-07-08 : Monterey, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1996
Summary:
The Surface Protected Ablator (SPA) is a lightweight and cost effective thermal protection for single use reentry capsules. It is characterised by a combination of load carrying structure, ablator and abrasion protection system. A simulation software has been developed to predict the thermal behaviour of the SPA during plasma wind tunnel tests and under atmospheric reentry conditions. Test samples have been exposed to different aerothermal heat fluxes. Test results have been used to calibrate the numerical model and to determine unknown properties of the ablative material. The calibrated model was applied for accurate flight predictions of the MIRKA reentry
Notes:
Vendor supplied data
Publisher Number:
961428
Access Restriction:
Restricted for use by site license

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