Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bypassRatio |
0.3:1
|
| gptkbp:category |
military aircraft engine
|
| gptkbp:compressionRatio |
axial
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:diameter |
0.69 m
|
| gptkbp:firstFlight |
1990
|
| gptkbp:fuelType |
gptkb:Jet-A1
|
| gptkbp:hasAfterburner |
yes
|
| gptkbp:hasConcept |
twin-spool
|
| https://www.w3.org/2000/01/rdf-schema#label |
Snecma M88
|
| gptkbp:intendedAircraft |
gptkb:Dassault_Rafale
|
| gptkbp:length |
3.5 m
|
| gptkbp:manufacturer |
gptkb:Snecma
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:relatedTo |
Snecma M53
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
50 kN
75 kN |
| gptkbp:usedIn |
gptkb:Dassault_Rafale
|
| gptkbp:weight |
897 kg
|
| gptkbp:bfsParent |
gptkb:Rafale_fighter_jets
|
| gptkbp:bfsLayer |
6
|