Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:combustor_type |
annular combustor
|
| gptkbp:compressor_type |
axial compressor
|
| gptkbp:control_system |
hydromechanical control system
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:country_of_origin |
gptkb:United_Kingdom
|
| gptkbp:design_uses |
gptkb:trainer_aircraft
|
| gptkbp:diameter |
3 ft 4 in
|
| gptkbp:engine_configuration |
turbojet
|
| gptkbp:first_flight |
gptkb:1960
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Viper 601
|
| gptkbp:length |
12 ft 6 in
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notable_users |
gptkb:Hawker_Siddeley_Hawk
|
| gptkbp:operational_history |
used in various aircraft
|
| gptkbp:propulsion |
6000 lbf
|
| gptkbp:successor |
gptkb:Rolls-Royce_Viper_632
|
| gptkbp:turbine_type |
single-stage turbine
|
| gptkbp:weight |
1200 lb
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Viper_632
|
| gptkbp:bfsLayer |
6
|