Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:combustor_type |
dual-spool
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
1.3 m
|
| gptkbp:engine |
Brayton cycle
|
| gptkbp:engine_configuration |
twin-spool
|
| gptkbp:first_flight |
gptkb:1981
|
| gptkbp:fuel_type |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
NK-32 engine
|
| gptkbp:length |
4.1 m
|
| gptkbp:manufacturer |
gptkb:Kuznetsov
|
| gptkbp:max_speed |
Mach 2.05
|
| gptkbp:number_of_engines |
2
|
| gptkbp:operational_range |
12,000 km
|
| gptkbp:propulsion |
13.9
25,000 kgf |
| gptkbp:related_aircraft |
gptkb:bomber
|
| gptkbp:service_ceiling |
15,000 m
|
| gptkbp:specific_impulse |
300 seconds
|
| gptkbp:type |
afterburning turbojet
|
| gptkbp:used_in |
gptkb:Tupolev_Tu-160
|
| gptkbp:weight |
1,800 kg
|
| gptkbp:bfsParent |
gptkb:Kuznetsov_Design_Bureau
|
| gptkbp:bfsLayer |
6
|