Accession Number : AD0378925

Title :   DEVELOPMENT OF A SUPERSONIC TRANSPORT AIRCRAFT ENGINE. PHASE II-C.

Descriptive Note : Final rept. 1 Jul 65-31 Dec 66.

Corporate Author : PRATT AND WHITNEY AIRCRAFT WEST PALM BEACH FLA FLORIDA RESEARCH AND DEVELOPMENT CENTER

Report Date : 11 JAN 1967

Pagination or Media Count : 486

Abstract : Contents: Engine Design; Engine Testing; Fan and High Compressor; Primary Combustor; Turbine; Augmentor; Exhaust System; Controls; Bearings and Seals; Fuels and Lubricants; Inlet System Compatibility; Noise; Mockups; Coordination; Maintainability; Value Engineering; Configuration Management; Quality Assurance; Reliability; Safety; Thrust Indicating System; and Economic Studies.

Descriptors :   (*JET TRANSPORT PLANES, TURBOFAN ENGINES), SUPERSONIC AIRCRAFT, COMMERCIAL PLANES, DESIGN, CAPTIVE TESTS, ENGINE FUEL SYSTEMS COMPONENTS, AVIATION SAFETY, DUCT INLETS, SEALS, BEARINGS, JET ENGINE FUELS, LUBRICATION, JET ENGINE NOISE, CONFIGURATION, COMPATIBILITY, MAINTAINABILITY, VALUE ENGINEERING, QUALITY CONTROL, RELIABILITY (U) PERFORMANCE(ENGINEERING), AXIAL FLOW FANS, AXIAL FLOW COMPRESSORS, COMBUSTION CHAMBERS, AXIAL FLOW TURBINES, THRUST AUGMENTATION, VARIABLE AREA NOZZLES, THRUST AUGMENTOR NOZZLES, THRUST REVERSAL

Subject Categories : Civilian Aircraft
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE