|
gptkbp:instanceOf
|
turboshaft engine
|
|
gptkbp:application
|
military helicopters
|
|
gptkbp:certifications
|
FAA_certified
|
|
gptkbp:compressionRatio
|
16:1
|
|
gptkbp:controls
|
digital electronic control
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design
|
modular
|
|
gptkbp:developer
|
ongoing
|
|
gptkbp:diameter
|
approximately 16 in
|
|
gptkbp:drivetrain
|
integrated reduction gearbox
|
|
gptkbp:emissionsStandard
|
low
|
|
gptkbp:energyEfficiency
|
high
|
|
gptkbp:engineConfiguration
|
free turbine
|
|
gptkbp:firstFlight
|
1980s
|
|
gptkbp:fuelType
|
Jet A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
T700-GE-701D
|
|
gptkbp:launchSite
|
starter-generator
|
|
gptkbp:length
|
approximately 48 in
|
|
gptkbp:maintenance
|
2,500 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:market
|
military and commercial
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operationalStatus
|
up to 1,000 °C
|
|
gptkbp:powerOutput
|
1,800 shp
|
|
gptkbp:propulsion
|
1,800 shp
4.5 shp/lb
|
|
gptkbp:relatedPatent
|
gptkb:T700-GE-701U
gptkb:T700-GE-701X
gptkb:T700-GE-701S
gptkb:T700-GE-701Z
gptkb:T700-GE-701P
gptkb:T700-GE-701V
gptkb:T700-GE-701Q
gptkb:T700-GE-701R
T700-GE-701E
T700-GE-700
T700-GE-701A
T700-GE-701B
T700-GE-701F
T700-GE-701G
T700-GE-701H
T700-GE-701I
T700-GE-701J
T700-GE-701K
T700-GE-701L
T700-GE-701M
T700-GE-701T
T700-GE-701Y
T700-GE-701N
T700-GE-701O
T700-GE-701W
|
|
gptkbp:reliability
|
high
|
|
gptkbp:services
|
high
|
|
gptkbp:successor
|
gptkb:T700-GE-701C
|
|
gptkbp:type
|
turbo-shaft engine
|
|
gptkbp:usedIn
|
gptkb:AH-64_Apache
gptkb:UH-60_Black_Hawk
|
|
gptkbp:weight
|
approximately 400 lb
|