Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
gptkb:General_Electric_I-40
|
| gptkbp:diameter |
33 in
|
| gptkbp:firstFlight |
1944
|
| gptkbp:length |
119 in
|
| gptkbp:manufacturer |
gptkb:Allison_Engine_Company
|
| gptkbp:notableFor |
first mass-produced American turbojet engine
|
| gptkbp:status |
retired
|
| gptkbp:thrust |
4,000 lbf
|
| gptkbp:type |
axial-flow turbojet
|
| gptkbp:usedInAircraft |
gptkb:McDonnell_F2H_Banshee
gptkb:Lockheed_F-94_Starfire gptkb:Lockheed_P-80_Shooting_Star gptkb:Northrop_F-89_Scorpion gptkb:McDonnell_FH_Phantom |
| gptkbp:weight |
1,820 lb
|
| gptkbp:bfsParent |
gptkb:P-80_Shooting_Star
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Allison J33
|