Accession Number : AD0376674

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

Descriptive Note : Monthly progress rept. no. 6, 1-31 Dec 65.

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

Report Date : 10 JAN 1966

Pagination or Media Count : 148

Descriptors :   (*JET TRANSPORT PLANES, *TURBOFAN ENGINES), (*SUPERSONIC AIRCRAFT, TURBOFAN ENGINES), DESIGN, CONSTRUCTION, COMBUSTION CHAMBERS, TURBOJET INLETS, AXIAL FLOW COMPRESSORS, TURBOJET EXHAUST NOZZLES, THRUST REVERSAL, VARIABLE AREA NOZZLES, AXIAL FLOW COMPRESSOR BLADES, THRUST AUGMENTOR NOZZLES, MANIFOLDS(ENGINES), BLEED SYSTEMS, DUCTS, HEATING, FUEL SYSTEMS, HYDRAULIC EQUIPMENT, FLIGHT CONTROL SYSTEMS, BEARINGS, SEALS, LUBRICANTS, JET ENGINE FUELS, GEARS, AXIAL FLOW TURBINES

Subject Categories : Transport Aircraft
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE