Accession Number : AD0486375

Title :   EXPERIMENTAL AND DESIGN STUDIES FOR TURBO-RAMJET COMBINATION ENGINE. VOLUME 1 - SPECIFICATIONS AND PERFORMANCE

Descriptive Note : Final rept.

Corporate Author : NORD AVIATION CHATILLON-SOUS-BAGNEUX (FRANCE)

Personal Author(s) : Chaulin, P ; Ravel, M ; Gozlan, A

PDF Url : AD0486375

Report Date : Jan 1966

Pagination or Media Count : 62

Abstract : Contents: GENERAL DESCRIPTION; DEFINITION OF THE X 81 COMBINED ENGINE; PERFORMANCE CHARACTERISTICS--Sea level static; flight air mass flow; flight without afterburning; flight with afterburning; Influence of the air inlet total pressure recovery; Influence of the nozzle thrust coefficient; Influence of air bleed; OVERALL DIMENSIONS - WEIGHT; INSTALLATION - HANDLING; AND COMBUSTION TESTS.

Descriptors :   *TURBORAMJET ENGINES, AFTERBURNERS, ALTITUDE, BLEED SYSTEMS, COMBUSTION, COMBUSTION CHAMBERS, CONTROL SYSTEMS, DUCTS, FRANCE, FUEL CONSUMPTION, GAS FLOW, HANDLING, JET ENGINE INLETS, MOUNTING BRACKETS, PERFORMANCE(ENGINEERING), PRESSURE, RECOVERY, SECONDARY FLOW, SPECIFICATIONS, THRUST, TURBOFAN ENGINES, TURBOJET EXHAUST NOZZLES, WEIGHT

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE