Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:compressionRatio |
centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
19 in
|
| gptkbp:family |
gptkb:Allison_Model_250
|
| gptkbp:firstFlight |
1970s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Allison 250-C20J
|
| gptkbp:length |
40.5 in
|
| gptkbp:manufacturer |
gptkb:Allison_Engine_Company
|
| gptkbp:marketedAs |
Rolls-Royce 250-C20J
|
| gptkbp:powerOutput |
420 shp
|
| gptkbp:successor |
Rolls-Royce 250-C20R
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedIn |
gptkb:Bell_206B_JetRanger_III
gptkb:Schweizer_330 |
| gptkbp:weight |
170 lb
|
| gptkbp:bfsParent |
gptkb:Bell_206B_JetRanger_III
|
| gptkbp:bfsLayer |
6
|