Statements (17)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:compressionRatio |
centrifugal-flow
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
33 in
|
| gptkbp:firstFlight |
1944
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Allison J33-A-41 turbojet
|
| gptkbp:length |
123 in
|
| gptkbp:manufacturer |
gptkb:Allison_Engine_Company
|
| gptkbp:status |
retired
|
| gptkbp:thrust |
4,600 lbf
|
| gptkbp:usedInAircraft |
gptkb:T-33_Shooting_Star
gptkb:Lockheed_F-94_Starfire gptkb:Lockheed_P-80_Shooting_Star |
| gptkbp:weight |
1,820 lb
|
| gptkbp:bfsParent |
gptkb:Mace_missile
|
| gptkbp:bfsLayer |
7
|