Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:cancellation_reason |
yes
|
| gptkbp:compressor_type |
axial
|
| gptkbp:design |
high bypass ratio
|
| gptkbp:diameter |
40 in
|
| gptkbp:engine_configuration |
twin-spool
|
| gptkbp:first_flight |
gptkb:1961
|
| gptkbp:fuel_capacity |
56 in
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
JT3 D series
|
| gptkbp:length |
12 ft 6 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:notable_users |
gptkb:Trans_World_Airlines
gptkb:United_Airlines gptkb:Eastern_Air_Lines gptkb:Pan_American_World_Airways |
| gptkbp:number_of_stages |
gptkb:3
|
| gptkbp:operational_history |
1961-1980s
|
| gptkbp:produces |
over 1,000
|
| gptkbp:propulsion |
18,000 lbf
|
| gptkbp:replaced_by |
gptkb:CF6_engine
|
| gptkbp:successor |
gptkb:JT8_D
|
| gptkbp:turbine_type |
single stage
|
| gptkbp:type |
gptkb:turbofan_engine
|
| gptkbp:used_in |
gptkb:Douglas_DC-8
|
| gptkbp:weight |
3,000 lb
|
| gptkbp:bfsParent |
gptkb:JT3_D-3_B
|
| gptkbp:bfsLayer |
6
|