Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
jet engine
|
| gptkbp:application |
military aviation
|
| gptkbp:controls |
FADEC
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:diameter |
1.1 m
|
| gptkbp:emissionsStandard |
compliant_with_ICAO_standards
|
| gptkbp:engineType |
axial
high bypass ratio |
| gptkbp:firstFlight |
1988
|
| gptkbp:fuelType |
gptkb:Jet_A-1
annular combustion chamber |
| https://www.w3.org/2000/01/rdf-schema#label |
Volvo RM12
|
| gptkbp:is_used_in |
Saab JAS 39 Gripen
|
| gptkbp:length |
3.8 m
|
| gptkbp:maintenance |
500 hours
|
| gptkbp:manufacturer |
gptkb:Volvo
|
| gptkbp:maximum_speed |
gptkb:Mach_2.0
|
| gptkbp:noise_level |
low
|
| gptkbp:operationalRange |
up to 15,000 m
|
| gptkbp:propulsion |
80 kN
|
| gptkbp:services |
approximately 4,000 hours
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:weight |
1,200 kg
|