Accession Number : AD0376671

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

Descriptive Note : Monthly progress rept. no. 12, 1-30 Jun 66.

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

Report Date : 08 JUL 1966

Pagination or Media Count : 125

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, Reliability.

Descriptors :   (*JET TRANSPORT PLANES, *TURBOFAN ENGINES), (*SUPERSONIC AIRCRAFT, TURBOFAN ENGINES), DESIGN, CONSTRUCTION, AXIAL FLOW COMPRESSORS, AXIAL FLOW FANS, JET ENGINE INLETS, BLEED SYSTEMS, MODEL TESTS, PERFORMANCE(ENGINEERING), VIBRATION, AXIAL FLOW TURBINES, COMBUSTION CHAMBERS, TURBINE BLADES, TURBOJET EXHAUST NOZZLES, FUEL SYSTEMS, IGNITION SYSTEMS, GAS GENERATING SYSTEMS, FUEL PUMPS, JET ENGINE NOISE, ATTENUATION, QUALITY CONTROL, THRUST AUGMENTOR NOZZLES (U) PLUG NOZZLES

Subject Categories : Transport Aircraft
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE