Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:certification |
civil certified
|
| gptkbp:countryOfOrigin |
gptkb:France
gptkb:United_Kingdom |
| gptkbp:diameter |
0.61 m
|
| gptkbp:features |
improved durability
modular design Full Authority Digital Engine Control (FADEC) |
| gptkbp:firstRun |
1998
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Adour Mk 951
|
| gptkbp:intendedUse |
gptkb:trainer_aircraft
|
| gptkbp:length |
2.9 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
gptkb:Turbomeca |
| gptkbp:part_of |
Rolls-Royce Adour family
|
| gptkbp:successor |
gptkb:Rolls-Royce_Adour_Mk_871
|
| gptkbp:thrust_(dry) |
6,500 lbf
|
| gptkbp:thrust_(with_afterburner) |
8,430 lbf
|
| gptkbp:usedInAircraft |
gptkb:HAL_Tejas
gptkb:BAE_Systems_Hawk |
| gptkbp:weight |
650 kg
|
| gptkbp:bfsParent |
gptkb:Hawk_T2_aircraft
gptkb:Hawk_167 gptkb:BAE_Systems_Hawk_T2 gptkb:Hawk_T2 |
| gptkbp:bfsLayer |
7
|