This specification establishes design and performance requirements for the Pratt and Whitney Aircraft JTF17A-21B 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 noted.
Jtf17a-21B Turbofan Engine Specification
1966
69 pages
Report
No indication
English
Jet & Gas Turbine Engines , Aircraft , Turbofan engines , Jet transport planes , Specifications , Supersonic aircraft , Jet engine fuels , Axial flow turbines , Commercial planes , Performance(Engineering) , Design , Standards , Aviation safety , Spare parts , Maintenance , Reliability , Vibration , Maneuverability , Test methods , Quality control , Storage , Jet engine noise , Nondestructive testing , Starting , Combustion , Jet engine inlets , Airframes , Supersonic transports , Tf-17 engines