Summary of engines built/designed by Lyul'ka
Model name |
Date |
Type |
Thrust (kg) / Power (eshp) |
Fitted to |
RTD-1/VDR-2 |
1938 |
Two-stage centrifugal compressor Turbojet |
500 kg estimated |
Test-bed only |
S-18/VDR-3 |
1945 |
Axial flow compressor Turbojet |
1,250 kg |
Gu-VRD project |
TR-1 |
1946 |
8-stage Axial flow compressor Turbojet |
1,300 kg |
Alekseyev I-21, Ilyushin Il-22, Sukhoi Su-10, Sukhoi Su-11 |
TR-1A |
1947 |
8-stage Axial flow compressor Turbojet |
1,500 kg |
|
TR-2 |
1947 |
|
|
projected growth version of TR-1 |
TR-3 and AL-5 |
1949 |
7-stage Axial-flow Turbojet |
4,600 kg (at qualification in 1950) |
Il-30, Il-46, Lavochkin Aircraft 190, Tu-86, Yak-1000, Su-17(1949), "Aircraft 150" |
TR-7 |
1950s |
supersonic compressor prototype of the AL-7 |
|
Prototype for AL-7 |
AL-7 |
1954 |
9-stage supersonic compressor Turbojet |
6,500 kg |
Il-54, Su-7B, Tu-98, Su |
AL-21 |
1961 |
14-stage Axial compressor with variable stator blades |
11,000 kg |
Yak-38, Tu-28/Tu-128, Su-17, Su-24 |
AL-31 |
1976 |
Twin-spool Turbofan 0.6 bypass ratio. |
13,300 kg |
Su-27, Su-30, Su-34, Su-35, Su-47 Berkut |