|
gptkbp:instanceOf
|
gptkb:piston_engine
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:civilianVersion
|
gptkb:General_Electric_CT7
|
|
gptkbp:combustorType
|
annular
|
|
gptkbp:compressionRatio
|
5-stage axial, 1-stage centrifugal
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:developedBy
|
gptkb:US_Army
|
|
gptkbp:diameter
|
19 in (48 cm)
|
|
gptkbp:family
|
gptkb:GE_T700/CT7
|
|
gptkbp:firstFlight
|
1973
|
|
gptkbp:fuelType
|
Jet-A, JP-4, JP-5, JP-8
|
|
gptkbp:introduced
|
1970s
|
|
gptkbp:length
|
41.4 in (105 cm)
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:notableFeature
|
modular design
ease of maintenance
high reliability
|
|
gptkbp:numberOfStages
|
2-stage high pressure, 2-stage power turbine
|
|
gptkbp:powerOutput
|
1,622–2,000 shp
|
|
gptkbp:primaryUser
|
gptkb:United_States_military
|
|
gptkbp:status
|
in production
|
|
gptkbp:successor
|
gptkb:General_Electric_T901
|
|
gptkbp:type
|
turboshaft
|
|
gptkbp:usedIn
|
gptkb:Bell_AH-1Z_Viper
gptkb:Sikorsky_UH-60_Black_Hawk
gptkb:Sikorsky_SH-60_Seahawk
gptkb:Boeing_AH-64_Apache
|
|
gptkbp:weight
|
456 lb (207 kg)
|
|
gptkbp:bfsParent
|
gptkb:General_Electric_T700-GE-401C
gptkb:SH-60F
gptkb:Sikorsky_UH-60_Black_Hawk
|
|
gptkbp:bfsLayer
|
6
|
|
http://www.w3.org/2000/01/rdf-schema#label
|
General Electric T700
|