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A leading edge heating array and a flat surface heating array: Final designA heating array is described for testing full-scale sections of the leading edge and lower fuselage surfaces of the shuttle. The heating array was designed to provide a tool for development and acceptance testing of leading edge segments and large flat sections of the main body thermal protection system. The array was designed using a variable length module concept to meet test requirements using interchangeable components from one test configuration in another configuration. Heat generating modules and heat absorbing modules were employed to achieve the thermal gradient around the leading edge. A support was developed to hold the modules to form an envelope around a variety of leading edges; to supply coolant to each module; the support structure and to hold the modules in the flat surface heater configuration. An optical pyrometer system mounted within the array was designed to monitor specimen surface temperatures without altering the test article's surface.
Document ID
19750022168
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
July 10, 1975
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-144390
JSC-09490
MDC-E1232
Report Number: NASA-CR-144390
Report Number: JSC-09490
Report Number: MDC-E1232
Accession Number
75N30241
Funding Number(s)
CONTRACT_GRANT: NAS9-14041
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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