General Electric T700-GE-701D turboshaft
GPTKB entity
Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
military helicopters
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressor_type |
5-stage axial, 1-stage centrifugal
|
| gptkbp:configuration |
axial-centrifugal flow
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
15.6 in
|
| gptkbp:family |
gptkb:General_Electric_T700
|
| gptkbp:fuelType |
Jet-A, JP-8
|
| gptkbp:improved_from |
gptkb:T700-GE-701C
|
| gptkbp:introducedIn |
2005
|
| gptkbp:length |
41.4 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:market |
gptkb:military
|
| gptkbp:powerOutput |
1,994 shp
|
| gptkbp:turbine_stages |
2-stage gas generator, 2-stage power turbine
|
| gptkbp:used_in |
gptkb:Sikorsky_UH-60_Black_Hawk
gptkb:Boeing_AH-64_Apache |
| gptkbp:weight |
456 lb
|
| gptkbp:bfsParent |
gptkb:UH-60M_Black_Hawk_helicopter
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric T700-GE-701D turboshaft
|