Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:alsoKnownAs |
gptkb:Lycoming_T55
|
| gptkbp:compressionRatio |
8.0:1
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
0.56 m
|
| gptkbp:firstFlight |
1955
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Honeywell T55
|
| gptkbp:length |
1.9 m
|
| gptkbp:manufacturer |
gptkb:Honeywell_Aerospace
gptkb:Lycoming_Engines |
| gptkbp:notableVariant |
gptkb:T55-L-714
|
| gptkbp:numberOfStages |
2
7 |
| gptkbp:powerOutput |
up to 4,800 shp
|
| gptkbp:status |
in production
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedBy |
gptkb:U.S._Army
|
| gptkbp:usedIn |
CH-47 Chinook
MH-47 Model 347 |
| gptkbp:weight |
408 kg
|
| gptkbp:bfsParent |
gptkb:Honeywell_T55-GA-714A
|
| gptkbp:bfsLayer |
6
|