Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
military helicopters
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
19 in
|
| gptkbp:family |
gptkb:General_Electric_T700
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:improves |
increased durability
higher power output |
| gptkbp:introducedIn |
1990s
|
| gptkbp:length |
42.5 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:notableRelease |
gptkb:T700-GE-701B
|
| gptkbp:numberOfStages |
2 gas generator, 2 power
5 axial, 1 centrifugal |
| gptkbp:powerOutput |
1,890 shp
|
| gptkbp:usedIn |
gptkb:Sikorsky_UH-60_Black_Hawk
gptkb:Sikorsky_SH-60_Seahawk gptkb:Boeing_AH-64_Apache |
| gptkbp:weight |
456 lb
|
| gptkbp:bfsParent |
gptkb:T700_engine
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
T700-GE-701C
|