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performance calculations for the IAE V2500-A1 aircraft engine
IAE V2500-A1 turbofan engine of 111.2 [KN] (24998 [lbf]) thrust
introduction : 1988 country : EU importance : ***
applications : Airbus A320-200
max. rating (take-off) : 111.2 [KN] (24998 [lbf], 11339 [kgf])
weight engine(s) dry : 2404.0 [kg] = 46.26 [N/kg]
General information :
by-pass ratio : 5.40 : 1
overall pressure ratio (OPR) : 35.8 : 1
rpm LP : 5650 [rpm]
rpm HP : 14950 [rpm]
axial flow engine
no water injection
arrangement : 1 Fan followed by :
LP compressor stages : 3 [ ]
HP compressor stages : 10 [ ]
HP turbine stages : 2 [ ]
LP turbine stages : 5 [ ]
stages : 1 + 3 + 10 + 2 + 5
turbine inlet temperature : 0 [K]
fan diameter : 168.0 [cm] engine diameter : 173.0 [cm]
air mass flow : 330 [kg/s]
design hours : 669 [hr] time between overhaul : 334 [hr]
estimated specific fuel consumption (cruise power) :55.4 [kg/KNh]
Literature :
Airbus-techdata-AC_A320_0322 (2).pdf
DISCLAIMER Above calculations are based on published data, they must be
regarded as indication not as facts.
Calculated performance and weight may not correspond with actual weights
and performances and are assumptions for which no responsibility can be taken.
Calculations are as accurate as possible, they can be fine-tuned when more data
is available, you are welcome to give suggestions and additional information
so we can improve our program. For copyright on drawings/photographs/
content please mail to below mail address
(c) B van der Zalm 22 October 2022 contact : info.aircraftinvestigation@gmail.com python 3.7.4