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Altitude performance evaluation of J71-A-11 turbojet engineData were obtained with five exhaust-nozzle areas and with the variable-area exhaust nozzle interlinked with the control system at conditions simulating flight at a Mach number of 0.8 and altitudes of 35,00 and 45,000 feet. Data simulating operation at zero flight Mach number at an altitude of 15,000 feet are also included. Engine component performance data are presented in addition to the overall engine performance.
Document ID
19930089055
Document Type
Other
Authors
Useller, James W
Pappas, George E
Date Acquired
August 16, 2013
Publication Date
March 30, 1956
Report/Patent Number
NACA-RM-E55J11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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