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

reportActive / Technical Report | Accession Number: AD0486375 | Open PDF

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.

Author(s):
Chaulin, P. ; Ravel, M. ; Gozlan, A.
Author Organization(s):
NORD AVIATION CHATILLON-SOUS-BAGNEUX (FRANCE)
Descriptive Note:
Final rept.
Supplementary Note:
See also Volume 2, AD486376
Pagination:
0062

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release
Distribution Statement:
Approved For Public Release; Distribution Is Unlimited.

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
5147/NIOBE-4/29/Z, AFAPL-TR-66-34-VOL-1
Contract/Grant Number(s):
AF 61(052)-750
Task Number(s):
301203
Project Number(s):
AF-3012
Monitor Series:
TR-66-34-VOL-1, AFAPL
 Subject Terms
Joint Capability Areas:
JCA_8_Building Partnerships; JCA_5_Command and Control; JCA_8.2_Shape; JCA_3_Force Application; JCA_3.2_Engagement; JCA_3.2.1_Kinetic Means; JCA_5.3_Planning; JCA_8.1_Communicate
Modernization Areas:
Hypersonics
Communities of Interest:
Air Platforms
Descriptor(s):
*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
Field(s)/Group(s):
Jet and Gas Turbine Engines
Keyword(s):
TF 106 ENGINES
Report Date:
1965 Jan 01