Accession Number : AD0370604

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

Descriptive Note : Monthly progress and administrative rept. for Jun 64.

Corporate Author : PRATT AND WHITNEY AIRCRAFT EAST HARTFORD CONN

Report Date : 15 JUL 1964

Pagination or Media Count : 8

Abstract : Contents: Analyses and Preliminary Design; Specifications; Compressor Development; Primary Combustion; Turbine Development; Augmentors; Exhaust System; Noise Reduction; Controls and Accessories; Bearing and Seal Development; Fuels; Lubricants; Inlets; Materials and Manufacturing Techniques; Operations and Economics; and Supporting Design Considerations.

Descriptors :   (*JET TRANSPORT PLANES, *SUPERSONIC AIRCRAFT) (U) TURBOJET ENGINES, PERFORMANCE(ENGINEERING), TURBOFAN ENGINES, AFTERBURNING, SPECIFICATIONS, COMPRESSORS, GEOMETRY, TURBOJET INLETS, COMBUSTION, TEST EQUIPMENT, TURBINE BLADES, HEAT TRANSFER, AIRFOILS, CASCADE STRUCTURES, EVAPOTRANSPIRATION, PLUG NOZZLES, ANECHOIC CHAMBERS, BEARINGS, SEALS, DESIGN, FATIGUE(MECHANICS)

Subject Categories : Transport Aircraft
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE