NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
NASA Lewis Research Center lean-, rich-burn materials test burner rigThe lean-, rich-burn materials test burner rig at NASA LeRC is used to evaluate the high temperature environmental durability of aerospace materials. The rig burns jet fuel and pressurized air, and sample materials can be subjected to both lean-burn and rich-burn environments. As part of NASA's Enabling Propulsion Materials (EPM) program, an existing rig was adapted to simulate the rich-burn quick-quench lean-burn (RQL) combustor concept which is being considered for the HSCT (high speed civil transport) aircraft. RQL materials requirements exceed that of current superalloys, thus ceramic matrix composites (CMC's) emerged as the leading candidate materials. The performance of these materials in the quasi reducing environment of the rich-burn section of the RQL is of fundamental importance to materials development. This rig was developed to conduct such studies, and its operation and capabilities are described.
Document ID
19940021638
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stearns, C. A.
(Sverdrup Technology, Inc. Brook Park, OH, United States)
Robinson, R. C.
(Sverdrup Technology, Inc. Brook Park, OH, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1994
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-CR-194437
E-8285
NAS 1.26:194437
Accession Number
94N26141
Funding Number(s)
CONTRACT_GRANT: NAS3-25266
PROJECT: RTOP 537-04-20
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available