Statements (32)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:alsoKnownAs |
gptkb:Allison_Model_250
|
| gptkbp:application |
gptkb:helicopter
fixed-wing aircraft |
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
13.8 in
|
| gptkbp:firstFlight |
1961
|
| gptkbp:introduced |
1960s
|
| gptkbp:length |
39.0 in
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Holdings
gptkb:Allison_Engine_Company |
| gptkbp:notableVariant |
M250-C20
M250-C30 M250-C40 M250-C47 |
| gptkbp:numberOfStages |
4
7 |
| gptkbp:powerOutput |
317 to 715 shp
|
| gptkbp:type |
turboprop
turboshaft |
| gptkbp:usedIn |
gptkb:OH-58_Kiowa
gptkb:Bell_206_JetRanger gptkb:MD_Helicopters_MD_500 gptkb:Schweizer_333 |
| gptkbp:weight |
170 lb
|
| gptkbp:bfsParent |
gptkb:Allison_Model_250
gptkb:Allison_T63 gptkb:Allison_250 gptkb:Rolls-Royce_M250-B17F gptkb:Allison_T63_turboshaft |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce M250
|