Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
5-stage axial, 1-stage centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
19 in
|
| gptkbp:family |
gptkb:General_Electric_T700
|
| gptkbp:firstFlight |
1973
|
| gptkbp:fuelType |
Jet-A, JP-4, JP-5, JP-8
|
| https://www.w3.org/2000/01/rdf-schema#label |
T700-GE-700
|
| gptkbp:length |
42.5 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:numberOfStages |
2-stage gas generator, 2-stage power turbine
|
| gptkbp:powerOutput |
1,622 shp
|
| gptkbp:relatedModel |
gptkb:T700-GE-401
gptkb:T700-GE-701 |
| gptkbp:status |
in service
|
| gptkbp:usedIn |
gptkb:SH-60_Seahawk
AH-64 Apache UH-60 Black Hawk |
| gptkbp:weight |
456 lb
|
| gptkbp:bfsParent |
gptkb:T700_engine
|
| gptkbp:bfsLayer |
6
|