Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
regional aircraft
|
| gptkbp:compressor_type |
axial compressor
|
| gptkbp:diameter |
approximately 3 ft
|
| gptkbp:engine_configuration |
twin-spool
|
| gptkbp:first_flight |
gptkb:1960
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Gem 42-1
|
| gptkbp:length |
approximately 10 ft
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:number_of_stages |
8 stages
|
| gptkbp:propulsion |
42 k N
|
| gptkbp:turbine_type |
high bypass ratio
|
| gptkbp:type |
gptkb:turbofan_engine
|
| gptkbp:used_in |
gptkb:Hawker_Siddeley_HS_748
|
| gptkbp:weight |
approximately 1,200 lb
|
| gptkbp:bfsParent |
gptkb:Sea_Lynx_helicopters
|
| gptkbp:bfsLayer |
6
|