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Accession Number:
AD0804528
Title:
JTF17A-21L TURBOFAN ENGINE SPECIFICATION
Corporate Author:
PRATT AND WHITNEY AIRCRAFT WEST PALM BEACH FL FLORIDA RESEARCH AND DEVELOPMENT CENTER
Report Date:
1966-08-08
Abstract:
This specification establishes design and performance requirements for the Pratt and Whitney Aircraft JTF17A-21L turbofan engine to be certificated in Phase 4 of the Supersonic Transport Program. Significant differences in the design and performance of the Phase 3 Flight Test Status engines for airplane flight testing are described.
Pages:
0094
Distribution Statement:
Approved for public release; distribution is unlimited. Document partially illegible.
Contract Number:
FA-SS-66-8
File Size:
5.72MB
