Statements (33)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:category |
military aircraft engine
axial-flow jet engine |
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:developedBy |
1970s
|
| gptkbp:diameter |
1.04 m
|
| gptkbp:firstFlight |
1972
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Tumansky R-29
|
| gptkbp:length |
4.39 m
|
| gptkbp:manufacturer |
gptkb:Tumansky
|
| gptkbp:numberOfStages |
2
9 |
| gptkbp:predecessor |
gptkb:Tumansky_R-27
|
| gptkbp:successor |
gptkb:Klimov_RD-33
|
| gptkbp:thrust |
81.4 kN
|
| gptkbp:thrustAfterburner |
112.8 kN
|
| gptkbp:type |
afterburning turbojet
|
| gptkbp:usedBy |
gptkb:Libyan_Air_Force
gptkb:Bulgarian_Air_Force gptkb:Indian_Air_Force gptkb:Chinese_Air_Force gptkb:Soviet_Air_Force gptkb:Egyptian_Air_Force gptkb:Iraqi_Air_Force gptkb:Syrian_Air_Force gptkb:North_Korean_Air_Force |
| gptkbp:usedInAircraft |
gptkb:Mikoyan_MiG-27
gptkb:Chengdu_J-7II gptkb:Mikoyan-Gurevich_MiG-23 |
| gptkbp:weight |
1,185 kg
|
| gptkbp:bfsParent |
gptkb:MiG-23
|
| gptkbp:bfsLayer |
6
|