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Demonstration of Advanced C/SiC Cooled RampUnder a NASA contract, SPS is evaluating its C/SiC to metal brazing technique for the development of light, composite, actively cooled panels. The program first consisted of defining a system applicable to the X-33 nozzle ramp. SPS then performed evaluation tests for tube, composite, and braze material selection, and for the adaptation of braze process parameters to the parts geometry. SPS is presently manufacturing a 250x60 millimeter squared specimen, including 10 metallic tubes, which will be cycled in the NASA/GRC-CELL-22 test bed under engine representative conditions.
Document ID
20020048698
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Bouquet, Clement
(Societe Nationale d'Etude et de Construction de Moteurs d'Aviation Bordeaux France)
Laithier, Frederic
(Societe Nationale d'Etude et de Construction de Moteurs d'Aviation Vernon France)
Lawrence, Timothy
(NASA Marshall Space Flight Center Huntsville, AL United States)
Eckel, Andrew
(NASA Glenn Research Center Cleveland, OH United States)
Munafo, Paul M.
Date Acquired
August 20, 2013
Publication Date
January 1, 2002
Subject Category
Composite Materials
Meeting Information
Meeting: 6th International Symposium on Propulsion for Space Transportation of the 21st Century
Location: Versailles
Country: France
Start Date: May 14, 2002
End Date: May 16, 2002
Funding Number(s)
CONTRACT_GRANT: NAS8-99112
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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