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.
Jtf17a-21L Turbofan Engine Specification
1966
67 pages
Report
Keine Angabe
Englisch
Jet & Gas Turbine Engines , Aircraft , Jet transport planes , Turbofan engines , Supersonic aircraft , Commercial planes , Specifications , Axially symmetric flow , Vibration , Airframes , Thrust , Gas flow , Jet engine inlets , Pressure , Deicing systems , Jet engine fuels , Airplane engine oils , Engine starters , Quality control , Design , Performance(Engineering) , Jtf-17 engines , Sea level , Supersonic transports
Jtf17a-21B Turbofan Engine Specification
NTIS | 1966
Turbofan engine and aircraft comprising turbofan engine
Europäisches Patentamt | 2021
|Springer Verlag | 2021
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