|
gptkbp:instanceOf
|
gptkb:helicopter
|
|
gptkbp:armament
|
none
|
|
gptkbp:capacity
|
up to 6 passengers
|
|
gptkbp:crew
|
1
|
|
gptkbp:design
|
conventional helicopter design
|
|
gptkbp:enginePower
|
1,000 shp
|
|
gptkbp:engineType
|
turboshaft
|
|
gptkbp:firstFlight
|
1960
|
|
gptkbp:fuelCapacity
|
500 L
|
|
gptkbp:height
|
3.8 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Sikorsky S-300
|
|
gptkbp:length
|
12.5 m
|
|
gptkbp:manufacturer
|
gptkb:Sikorsky_Aircraft_Corporation
|
|
gptkbp:maxSpeed
|
250 km/h
|
|
gptkbp:maxTakeoffWeight
|
2,500 kg
|
|
gptkbp:notableFeature
|
high maneuverability
reliable performance
easy maintenance
versatile mission capabilities
|
|
gptkbp:numberBuilt
|
200
|
|
gptkbp:numberOfEpisodes
|
1
|
|
gptkbp:primaryUser
|
gptkb:United_States_Air_Force
gptkb:United_States_Army
gptkb:United_States_Navy
|
|
gptkbp:productionYears
|
1960-1970
|
|
gptkbp:propulsion
|
single main rotor and tail rotor
|
|
gptkbp:range
|
600 km
|
|
gptkbp:relatedAircraft
|
gptkb:Boeing_CH-47_Chinook
gptkb:Eurocopter_AS350
gptkb:Bell_206
gptkb:Sikorsky_S-400
AgustaWestland AW109
|
|
gptkbp:role
|
utility helicopter
|
|
gptkbp:rotorDiameter
|
10.7 m
|
|
gptkbp:services
|
4,500 m
|
|
gptkbp:successor
|
gptkb:Sikorsky_S-400
|
|
gptkbp:usedBy
|
military
civilian
|
|
gptkbp:variant
|
S-300C
S-300A
S-300B
|
|
gptkbp:weight
|
1,500 kg
|