|
gptkbp:instanceOf
|
gptkb:helicopter
|
|
gptkbp:armament
|
none
|
|
gptkbp:avionics
|
modern navigation systems
|
|
gptkbp:constructionMaterial
|
aluminum alloy
|
|
gptkbp:controls
|
fly-by-wire
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Sikorsky_Aircraft_Corporation
twin-engine
|
|
gptkbp:developer
|
gptkb:Sikorsky_S-300_series
|
|
gptkbp:emergencyServices
|
crashworthy design
|
|
gptkbp:engine
|
gptkb:General_Electric_T58
|
|
gptkbp:engineType
|
turboshaft
|
|
gptkbp:exhibits
|
airshows and museums
|
|
gptkbp:firstFlight
|
1980
1995
|
|
gptkbp:fuelCapacity
|
1,200 L
|
|
gptkbp:height
|
4.57 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Sikorsky S-3100
|
|
gptkbp:influences
|
design_of_future_Sikorsky_helicopters
|
|
gptkbp:introduced
|
1980
|
|
gptkbp:landingGear
|
retractable
|
|
gptkbp:legacy
|
contribution to helicopter design.
|
|
gptkbp:length
|
15.24 m
|
|
gptkbp:manufacturer
|
gptkb:Sikorsky_Aircraft_Corporation
|
|
gptkbp:market
|
1980
civil and military
|
|
gptkbp:maxSpeed
|
250 km/h
|
|
gptkbp:maxTakeoffWeight
|
3,175 kg
|
|
gptkbp:notableFeature
|
dual rotor system
few minor accidents
|
|
gptkbp:numberBuilt
|
10
|
|
gptkbp:operationalHistory
|
used in various roles
|
|
gptkbp:passengerCapacity
|
6
1,500 kg
|
|
gptkbp:performance
|
high maneuverability
|
|
gptkbp:primaryUser
|
gptkb:U.S._Army
|
|
gptkbp:productionCompany
|
1980-1985
|
|
gptkbp:propulsion
|
twin-engine configuration
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:relatedAircraft
|
gptkb:Sikorsky_S-76
gptkb:Sikorsky_S-92
gptkb:Sikorsky_S-300
|
|
gptkbp:retirementYear
|
1990
|
|
gptkbp:role
|
transport
|
|
gptkbp:rotorDiameter
|
13.41 m
|
|
gptkbp:safetyFeatures
|
generally positive
|
|
gptkbp:services
|
4,600 m
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Sikorsky_S-300C
|
|
gptkbp:type
|
utility helicopter
|
|
gptkbp:variant
|
S-3100A
S-3100B
S-3100C
|