Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
jet engine
|
| gptkbp:aircraft |
gptkb:Tupolev_family
|
| gptkbp:application |
military aircraft
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:design |
gptkb:Vladimir_Tumansky
|
| gptkbp:diameter |
1.1 m
|
| gptkbp:engineConfiguration |
turbojet
|
| gptkbp:engineType |
axial
single_spool |
| gptkbp:firstFlight |
1950s
|
| gptkbp:fuel_capacity |
0.85 kg/kN·h
|
| gptkbp:fuelType |
annular
kerosene |
| https://www.w3.org/2000/01/rdf-schema#label |
Tumansky R-15
|
| gptkbp:is_used_in |
gptkb:Tupolev_Tu-16
|
| gptkbp:length |
4.2 m
|
| gptkbp:manufacturer |
Tumansky
|
| gptkbp:operational_status |
gptkb:Soviet_Air_Force
|
| gptkbp:operationalRange |
high_altitude
|
| gptkbp:propulsion |
15,000 lbf
|
| gptkbp:related_engine |
Brayton_cycle
|
| gptkbp:retired |
1990s
|
| gptkbp:successor |
gptkb:Tumansky_R-25
|
| gptkbp:type |
turbojet engine
|
| gptkbp:weight |
1,200 kg
|