Accession Number : AD0378634

Title :   COMMERCIAL SUPERSONIC TRANSPORT PROGRAM. PHASE II-C. PROPULSION SYSTEM PERFORMANCE SPECIFICATION. GENERAL ELECTRIC GE4/J5G ENGINE INSTALLATION.

Descriptive Note : Interim aircraft performance assessment rept.

Corporate Author : BOEING CO RENTON WASH

Report Date : 15 NOV 1965

Pagination or Media Count : 26

Abstract : This specification defines the installed performance for the 475-pound-per-second size General Electric Company GE4/J5G engine in the Boeing Model 733-390 airplane and specifies the estimated inlet and nozzle drag values used for the determination of the airplane performance characteristics. System performance requirements established herein are design objectives to be applied in the prototype airplanes. Application of these requirements to production airplane design will be established after prototype flight testing. (Author).

Descriptors :   (*JET TRANSPORT PLANES, TURBOJET ENGINES), (*TURBOJET ENGINES, SUPERSONIC AIRCRAFT), DESIGN, SPECIFICATIONS, PERFORMANCE(ENGINEERING), ENGINE AIR SYSTEMS COMPONENTS, JET ENGINE INLETS, JET ENGINE NACELLES, TURBOJET EXHAUST NOZZLES, BLEED SYSTEMS, DRAG, TAKEOFF, CLIMBING, SUPERSONIC FLIGHT, SUBSONIC CHARACTERISTICS, GRAPHICS (U) THRUST REVERSAL

Subject Categories : Transport Aircraft
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE