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Increased Re-Entry Vehicle Thermal Protection Requirements Due to Surface Roughness G. E. Re-entry Systems Operations Philadelphia, PA

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Nestler, Donald E., author.
Conference Name:
Intersociety Conference on Environmental Systems (1985-07-15 : San Francisco, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1985
Summary:
A survey is presented of recent experimental data, correlations, and prediction methods for the effects of surface roughness on re-entry vehicle aerodynamic heating, as related to thermal-protection requirements. Regions of concern are the nosetip and frustum; in each case, the primary source of surface roughness is the ablative response of non-homogenous heat-protection materials. Numerical examples are given to illustrate the quantitative effects of surface roughness on thermal-protection requirements for typical re-entry vehicles. Several correlations are used to demonstrate the wide variation in predictions that can result. The paper closes with an assessment of critical technology needs in this field
Notes:
Vendor supplied data
Publisher Number:
851381
Access Restriction:
Restricted for use by site license

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