Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
military helicopters
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
15.6 in
|
| gptkbp:firstFlight |
1978
|
| gptkbp:fuelType |
gptkb:gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
T700-GE-701B
|
| gptkbp:length |
42.5 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:numberOfStages |
2
5 axial, 1 centrifugal |
| gptkbp:partOf |
T700 engine family
|
| gptkbp:powerOutput |
1,800 shp
|
| gptkbp:predecessor |
gptkb:T700-GE-700
|
| gptkbp:successor |
gptkb:T700-GE-701C
|
| gptkbp:usedIn |
gptkb:SH-60_Seahawk
AH-64 Apache UH-60 Black Hawk |
| gptkbp:weight |
456 lb
|
| gptkbp:bfsParent |
gptkb:T700-GE-701C
|
| gptkbp:bfsLayer |
7
|