|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:application
|
gptkb:helicopter
fixed-wing aircraft
|
|
gptkbp:civilianDesignation
|
CT7
|
|
gptkbp:compressionRatio
|
axial-centrifugal
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:diameter
|
15.6 in (396 mm)
|
|
gptkbp:family
|
gptkb:GE_T700
|
|
gptkbp:firstFlight
|
1973
|
|
gptkbp:fuelType
|
gptkb:JP-4
gptkb:JP-8
gptkb:Jet-A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
T700 engine
|
|
gptkbp:introduced
|
1978
|
|
gptkbp:length
|
42.5 in (1,080 mm)
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:marketedAs
|
gptkb:GE_CT7
gptkb:GE_T700
|
|
gptkbp:militaryDesignation
|
gptkb:T700
|
|
gptkbp:notableFeature
|
modular design
ease of maintenance
high reliability
|
|
gptkbp:notableUser
|
gptkb:United_States_Air_Force
gptkb:United_States_Army
gptkb:United_States_Navy
civilian operators
international military forces
|
|
gptkbp:notableVariant
|
gptkb:T700-GE-401
gptkb:T700-GE-401C
gptkb:T700-GE-700
gptkb:T700-GE-701
gptkb:T700-GE-701C
gptkb:T700-GE-701D
CT7-2
CT7-8
|
|
gptkbp:numberOfStages
|
2 gas generator, 2 power
5 axial, 1 centrifugal
|
|
gptkbp:powerOutput
|
1,622 shp (1,210 kW) to 2,000 shp (1,491 kW)
|
|
gptkbp:status
|
in production
|
|
gptkbp:thrust
|
1,622 shp to 2,000 shp
|
|
gptkbp:type
|
turboshaft
|
|
gptkbp:usedIn
|
gptkb:Sikorsky_S-70
gptkb:AgustaWestland_AW101
gptkb:Bell_AH-1Z_Viper
gptkb:SH-60_Seahawk
AH-64 Apache
UH-60 Black Hawk
|
|
gptkbp:weight
|
456 lb (207 kg)
|
|
gptkbp:bfsParent
|
gptkb:GE_Aerospace
|
|
gptkbp:bfsLayer
|
5
|