This specification describes the aircraft engine installation. The essential physical and functional characteristics are noted and the design requirements are specified in some detail. Ground and flight tests which will ensure that the installation is satisfactory are established. The specific engine installation covered is the GE4/J5G. (Author)
Commercial Supersonic Transport Program. Phase II-C. Interim Aircraft Performance Assessment Report. Aircraft Engine Installation Performance Specification
1965
35 pages
Report
No indication
English
Jet & Gas Turbine Engines , Aircraft , Jet transport planes , Turbojet engines , Supersonic aircraft , Commercial planes , Installation , Specifications , Turbojet exhaust nozzles , Bleed systems , Engine mounts , Control systems , Reliability , Safety , Jet engine fairings , Turbojet inlets , Lubrication , Wiring diagrams , Ge-4/j-5 engines , Supersonic transports