Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:combustor_type |
annular
|
| gptkbp:compressor_type |
axial
|
| gptkbp:control_system |
gptkb:FADEC
|
| gptkbp:country_of_origin |
gptkb:Sweden
|
| gptkbp:diameter |
1.1 m
|
| gptkbp:engine |
Brayton cycle
|
| gptkbp:first_flight |
gptkb:1988
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Volvo RM12
|
| gptkbp:length |
3.8 m
|
| gptkbp:manufacturer |
gptkb:Volvo
|
| gptkbp:max_speed |
Mach 2.0
|
| gptkbp:operational_range |
1,500 km
|
| gptkbp:propulsion |
80 k N
|
| gptkbp:service_ceiling |
15,000 m
|
| gptkbp:turbine_type |
high bypass ratio
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:used_in |
gptkb:Saab_JAS_39_Gripen
|
| gptkbp:weight |
1,200 kg
|
| gptkbp:bfsParent |
gptkb:Saab_JAS_39_Gripen
|
| gptkbp:bfsLayer |
4
|