Tumansky R-13

Tumansky R-13

Tumansky R-13 designed by Sergei Alekseevich Gavrilov is a turbojet engine.

Background

The Tumansky R-13 is a development of the successful Tumansky R-11 engine. It is a two-spool axial-flow turbojet featuring a new 5-stage high-pressure compressor, new combustion chamber design to facilitate restarting the engine at high altitudes, new afterburner, and greater use of titanium components. It is used by MiG-21M, MF, SM, and SMT, and Sukhoi Su-15M and TM. R-13 is also built under license in China as LM WP13.

pecifications (R-13-300)

jetspecs

type=Afterburning turbojet
length=4,605 mm (181.3 in)
diameter=1,095 mm (43.1 in)
weight=1,205 kg (2,656 lb)
compressor=Two-spool axial compressor
combustion=
turbine=
fueltype=
oilsystem=
power=
thrust=
*39.9 kN (8,970 lbf) military thrust
*63.7 kN (14,320 lbf) with afterburner
compression=8.9:1
aircon=
turbinetemp=1,005 °C (1,840 °F)
fuelcon=
specfuelcon=
*95 kg/(h·kN) (0.93 lb/(h·lbf)) at idle
*213 kg/(h·kN) (2.09 lb/(h·lbf)) with afterburner
power/weight=
thrust/weight=52.8 N/kg (5.4:1)


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