Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:certification |
FAA type certified
|
| gptkbp:configuration |
axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
22.5 inches
|
| gptkbp:family |
gptkb:Honeywell_T55
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Honeywell T55-GA-714A
|
| gptkbp:length |
79.5 inches
|
| gptkbp:manufacturer |
gptkb:Honeywell_Aerospace
|
| gptkbp:notableRelease |
gptkb:Honeywell_T55-L-712
|
| gptkbp:numberOfStages |
14
4 |
| gptkbp:powerOutput |
4,868 shaft horsepower
|
| gptkbp:usedIn |
gptkb:MH-47G_Chinook
gptkb:Boeing_CH-47_Chinook |
| gptkbp:weight |
1,200 pounds
|
| gptkbp:bfsParent |
gptkb:MH-47_Chinook
|
| gptkbp:bfsLayer |
5
|