Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:compressionRatio |
8.8:1
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
13.8 in
|
| gptkbp:family |
gptkb:Rolls-Royce_M250
|
| gptkbp:firstProduced |
1990s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce M250-B17F
|
| gptkbp:length |
40.6 in
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:numberOfStages |
2
7 |
| gptkbp:powerOutput |
450 shp
|
| gptkbp:type |
turboshaft
|
| gptkbp:used_in |
gptkb:MD_Helicopters_MD_500
gptkb:Bell_206L-4_LongRanger gptkb:Schweizer_333 |
| gptkbp:weight |
170 lb
|
| gptkbp:bfsParent |
gptkb:Grob_G_120TP
|
| gptkbp:bfsLayer |
6
|