Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:combustor_type |
annular combustor
|
| gptkbp:compressor_type |
axial compressor
|
| gptkbp:diameter |
0.9 m
|
| gptkbp:engine_configuration |
twin-spool
|
| gptkbp:first_flight |
gptkb:1978
|
| gptkbp:fuel_economy |
0.85 kg/k N/h
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
SNECMA M53
|
| gptkbp:length |
3.8 m
|
| gptkbp:manufacturer |
gptkb:SNECMA
|
| gptkbp:max_speed |
Mach 2.2
|
| gptkbp:notable_users |
gptkb:United_Arab_Emirates_Air_Force
gptkb:Qatar_Air_Force gptkb:Indian_Air_Force gptkb:French_Air_Force |
| gptkbp:propulsion |
50 k N
|
| gptkbp:related_aircraft |
gptkb:fighter_aircraft
|
| gptkbp:service_entry |
gptkb:1980
|
| gptkbp:turbine_type |
single-stage turbine
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:used_in |
gptkb:Dassault_Mirage_2000
|
| gptkbp:weight |
about 1,200 kg
|
| gptkbp:bfsParent |
gptkb:Dassault_Mirage_2000
gptkb:Mirage_2000 |
| gptkbp:bfsLayer |
5
|