Accession Number : AD0376664

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

Descriptive Note : Monthly progress rept. no. 3, 1-30 Sep 65.

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

Report Date : 08 OCT 1965

Pagination or Media Count : 58

Descriptors :   (*JET TRANSPORT PLANES, *TURBOFAN ENGINES), (*SUPERSONIC AIRCRAFT, TURBOFAN ENGINES), DESIGN, CONSTRUCTION, AXIAL FLOW FANS, AXIAL FLOW COMPRESSORS, COMBUSTION CHAMBERS, TURBOJET INLETS, INLET DUCTS, FUEL NOZZLES, HEATING, AXIAL FLOW TURBINES, TURBOJET EXHAUST NOZZLES, THRUST REVERSAL, MODEL TESTS, PERFORMANCE(ENGINEERING), COMPATIBILITY, JET ENGINE FUELS, LUBRICATION, THRUST AUGMENTOR NOZZLES, CASCADE STRUCTURES, TURBINE BLADES

Subject Categories : Transport Aircraft
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE