NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Advanced Turbine Technology Applications Project (ATTAP)ATTAP activities were highlighted by test bed engine design and development activities; ceramic component design; materials and engine component characterization; ceramic component process development and fabrication; component rig testing; and test bed engine fabrication and testing. Specifically, ATTAP aims to develop and demonstrate the technology of structural ceramics that have the potential for competitive automotive engine life cycle cost and for operating for 3500 hours in a turbine engine environment at temperatures up to 1371 C (2500 F).
Document ID
19920016406
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 6, 2013
Publication Date
December 1, 1991
Subject Category
Mechanical Engineering
Report/Patent Number
EDR-15593
DOE/NASA 0336-3
NAS 1.26:189142
NASA-CR-189142
Report Number: EDR-15593
Report Number: DOE/NASA 0336-3
Report Number: NAS 1.26:189142
Report Number: NASA-CR-189142
Accession Number
92N25649
Funding Number(s)
CONTRACT_GRANT: DEN3-336
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available