Accession Number : AD0376672

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

Descriptive Note : Monthly progress rept. no. 13, 1-31 Jul 66.

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

Report Date : 10 AUG 1966

Pagination or Media Count : 203

Abstract : Contents: Engine Design; Engine Test; 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; and Reliability.

Descriptors :   (*JET TRANSPORT PLANES, *TURBOFAN ENGINES), (*SUPERSONIC AIRCRAFT, TURBOFAN ENGINES), DESIGN, CONSTRUCTION, MODEL TESTS, PERFORMANCE(ENGINEERING), AXIAL FLOW COMPRESSORS, TURBOJET INLETS, DUCT INLETS, HEATING, AXIAL FLOW TURBINES, TURBINE BLADES, TURBOJET EXHAUST NOZZLES, THRUST REVERSAL, COMBUSTION CHAMBERS, JET ENGINE NOISE, ATTENUATION, JET ENGINE FUELS, FUEL SYSTEMS, LUBRICANTS, HYDRAULIC EQUIPMENT, BEARINGS, SEALS, IGNITION SYSTEMS, THRUST AUGMENTOR NOZZLES, AERODYNAMIC CHARACTERISTICS

Subject Categories : Transport Aircraft
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE