Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
military and civilian aircraft
|
| gptkbp:compressor_type |
axial
|
| gptkbp:configuration |
twin-spool
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
2.5 ft
1.8 ft |
| gptkbp:engine |
Brayton cycle
|
| gptkbp:first_flight |
gptkb:1970
|
| gptkbp:fuel_economy |
0.5 lb/lbf/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric CT7-8 A
|
| gptkbp:length |
4.5 ft
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:operational_range |
30,000 to 40,000 ft
|
| gptkbp:propulsion |
3,000 lbf
|
| gptkbp:successor |
gptkb:General_Electric_CT7-9_B
|
| gptkbp:turbine_type |
high bypass ratio
|
| gptkbp:used_in |
gptkb:Bell_Boeing_V-22_Osprey
|
| gptkbp:weight |
1,200 lb
|
| gptkbp:bfsParent |
gptkb:Sikorsky_S-92
|
| gptkbp:bfsLayer |
5
|