col : model name | date | type | thrust (kg) / power (eshp) | fitted to row 1 : rtd-1/vdr-2 | 1938 | two-stage centrifugal compressor turbojet | 500 kg estimated | test-bed only row 2 : s-18/vdr-3 | 1945 | axial flow compressor turbojet | 1,250 kg | gu-vrd project row 3 : tr-1 | 1946 | 8-stage axial flow compressor turbojet | 1,300 kg | alekseyev i-21, ilyushin il-22, su row 4 : tr-1a | 1947 | 8-stage axial flow compressor turbojet | 1,500 kg | nan row 5 : tr-2 | 1947 | nan | nan | projected growth version of tr-1 row 6 : 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 row 7 : tr-7 | 1950s | supersonic compressor prototype of the al-7 | nan | prototype for al-7 row 8 : al-7 | 1954 | 9-stage supersonic compressor turbojet | 6,500 kg | il-54, su-7b, tu-98, su row 9 : al-21 | 1961 | 14-stage axial compressor with variable stator blades | 11,000 kg | yak-38, tu-28/tu-128, su-17 row 10 : al-31 | 1976 | twin-spool turbofan 0.6 bypass ratio. | 13,300 kg | su-27, su-30, su-34, su-35,
what are the thrust powers of the models?
500 kg estimated, 1,250 kg, 1,300 kg, 1,500 kg, 4,600 kg (at qualification in 1950), 6,500 kg, 11,000 kg, 13,300 kg
Model name Date Type Thrust (kg) / Power (eshp) Fitted to
what are the thrust powers of the models?
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, Su
TR-1A 1947 8-stage Axial flow compressor Turbojet 1,500 kg nan
TR-2 1947 nan nan 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
TR-7 1950s supersonic compressor prototype of the AL-7 nan 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
AL-31 1976 Twin-spool Turbofan 0.6 bypass ratio. 13,300 kg Su-27, Su-30, Su-34, Su-35,
500 kg estimated 1,250 kg 1,300 kg 1,500 kg 4,600 kg (at qualification in 1950) 6,500 kg 11,000 kg 13,300 kg
what are the thrust powers of the models? || 