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JTF17A-21L TURBOFAN ENGINE SPECIFICATION
PRATT AND WHITNEY AIRCRAFT WEST PALM BEACH FL FLORIDA RESEARCH AND DEVELOPMENT CENTER
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.
Approved for public release; distribution is unlimited. Document partially illegible.