Statements (65)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
jet engine
|
| gptkbp:aircraft |
Mikoyan-Gurevich MiG-21-2000E
Mikoyan-Gurevich MiG-21-2000G Mikoyan-Gurevich MiG-21-2000O Mikoyan-Gurevich MiG-21-2000U Mikoyan-Gurevich_MiG-21-2000 Mikoyan-Gurevich_MiG-21-2000A Mikoyan-Gurevich_MiG-21-2000B Mikoyan-Gurevich_MiG-21-2000C Mikoyan-Gurevich_MiG-21-2000D Mikoyan-Gurevich_MiG-21-2000F Mikoyan-Gurevich_MiG-21-2000H Mikoyan-Gurevich_MiG-21-2000I Mikoyan-Gurevich_MiG-21-2000J Mikoyan-Gurevich_MiG-21-2000K Mikoyan-Gurevich_MiG-21-2000L Mikoyan-Gurevich_MiG-21-2000M Mikoyan-Gurevich_MiG-21-2000N Mikoyan-Gurevich_MiG-21-2000P Mikoyan-Gurevich_MiG-21-2000Q Mikoyan-Gurevich_MiG-21-2000R Mikoyan-Gurevich_MiG-21-2000S Mikoyan-Gurevich_MiG-21-2000T Mikoyan-Gurevich_MiG-21-2000V Mikoyan-Gurevich_MiG-21-2000W Mikoyan-Gurevich_MiG-21-2000X Mikoyan-Gurevich_MiG-21-2000Y Mikoyan-Gurevich_MiG-21-2000Z Mikoyan-Gurevich_MiG-21-93 Mikoyan-Gurevich_MiG-21M Mikoyan-Gurevich_MiG-21bis Mikoyan-Gurevich_MiG-21F-13 Mikoyan-Gurevich_MiG-21MF Mikoyan-Gurevich_MiG-21PF Mikoyan-Gurevich_MiG-21PFL Mikoyan-Gurevich_MiG-21R Mikoyan-Gurevich_MiG-21S Mikoyan-Gurevich_MiG-21UM Mikoyan-Gurevich_MiG-21bisD |
| gptkbp:airlines |
60 kg/s
|
| gptkbp:application |
military aviation
|
| gptkbp:compressionRatio |
8:1
|
| gptkbp:diameter |
0.9 m
|
| gptkbp:engineConfiguration |
single-spool
|
| gptkbp:engineType |
axial turbine
|
| gptkbp:firstFlight |
1955
|
| gptkbp:fuel_capacity |
0.85 kg/kN·h
|
| gptkbp:fuelType |
kerosene
annular combustor |
| https://www.w3.org/2000/01/rdf-schema#label |
Tumansky R-11F-300
|
| gptkbp:introduced |
1955
|
| gptkbp:is_used_in |
gptkb:Mikoyan-Gurevich_MiG-21
|
| gptkbp:length |
3.8 m
|
| gptkbp:manufacturer |
Tumansky
|
| gptkbp:notable_feature |
R-11F-300A
|
| gptkbp:number_of_stages |
3
|
| gptkbp:operationalHistory |
used_in_Soviet_Air_Force
|
| gptkbp:origin |
gptkb:Soviet_Union
|
| gptkbp:propulsion |
50 kN
|
| gptkbp:related_engine |
Brayton_cycle
|
| gptkbp:replacedBy |
R-13F-300
|
| gptkbp:retired |
1990s
|
| gptkbp:successor |
Tumansky_R-13
|
| gptkbp:type |
afterburning turbojet
|
| gptkbp:weight |
800 kg
|