Snecma M53-P2 afterburning turbofan
GPTKB entity
Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bypassRatio |
0.53
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:diameter |
1.02 m
|
| gptkbp:engineType |
afterburning turbofan
|
| gptkbp:firstFlight |
1970s
|
| gptkbp:length |
4.96 m
|
| gptkbp:manufacturer |
gptkb:Snecma
|
| gptkbp:numberOfAxles |
single-shaft
|
| gptkbp:status |
in service
|
| gptkbp:successor |
gptkb:Snecma_M88
|
| gptkbp:thrust |
64 kN
95 kN |
| gptkbp:usedInAircraft |
gptkb:Dassault_Mirage_2000
|
| gptkbp:weight |
1,520 kg
|
| gptkbp:bfsParent |
gptkb:Mirage_2000C
|
| gptkbp:bfsLayer |
6
|
| http://www.w3.org/2000/01/rdf-schema#label |
Snecma M53-P2 afterburning turbofan
|