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Preliminary Altitude Performance Data of J71-A2 Turbojet Engine AfterburnerThe performance and operational characteristics of the J71-A2 turbojet-engine afterburner were investigated for a range of altitudes from 23,000 to 60,000 feet at a flight Mach number of 0,9 and at flight Mach numbers of 0.6, 0.9, and 1.0 at an altitude of 45,000 feet. The combustion performance and altitude operational limits, as well as the altitude starting characteristics have been determined.
Document ID
20090021752
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Useller, James W. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Mallett, William E. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
October 7, 1954
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NACA-RM-SE54J06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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