Turbo-Union RB199-34R Mk 103
GPTKB entity
Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:diameter |
0.86 m
|
| gptkbp:firstFlight |
1972
|
| gptkbp:length |
3.98 m
|
| gptkbp:manufacturer |
Turbo-Union
|
| gptkbp:numberOfAxles |
3
|
| gptkbp:numberOfSpools |
3
|
| gptkbp:relatedTo |
gptkb:Turbo-Union_RB199
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
~40 kN
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedIn |
gptkb:aircraft
|
| gptkbp:weight |
~1,090 kg
|
| gptkbp:bfsParent |
gptkb:2_×_Turbo-Union_RB199-34R_Mk_103_turbofans
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Turbo-Union RB199-34R Mk 103
|