Accession Number : AD0376675

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

Descriptive Note : Monthly progress rept. no. 8, 1-28 Feb 66.

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

Report Date : 10 MAR 1966

Pagination or Media Count : 258

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, AXIAL FLOW COMPRESSORS, COMBUSTION CHAMBERS, AXIAL FLOW TURBINES, THRUST AUGMENTOR NOZZLES, TURBOJET EXHAUST NOZZLES, THRUST REVERSAL, TURBOJET INLETS, COMPATIBILITY, JET ENGINE NOISE, ATTENUATORS, BEARINGS, SEALS, JET ENGINE FUELS, LUBRICANTS, LUBRICATION, HYDRAULIC EQUIPMENT, QUALITY CONTROL, RELIABILITY, MANUFACTURING, AXIAL FLOW FANS, SHROUD RINGS

Subject Categories : Transport Aircraft
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE