|
gptkbp:instanceOf
|
gptkb:helicopter
|
|
gptkbp:armament
|
none
|
|
gptkbp:avionics
|
basic navigation system
|
|
gptkbp:controls
|
fly-by-wire
|
|
gptkbp:crew
|
1
|
|
gptkbp:currentStatus
|
retired
|
|
gptkbp:design
|
gptkb:United_States
dual rotor system
|
|
gptkbp:enginePower
|
1,200 hp
|
|
gptkbp:engineType
|
turbine engine
|
|
gptkbp:firstFlight
|
1960
|
|
gptkbp:fuelCapacity
|
100 gallons
|
|
gptkbp:height
|
12 ft
|
|
gptkbp:helicopterCapacity
|
gptkb:tandem_rotor
|
|
gptkbp:historicalSignificance
|
first tandem rotor helicopter in service
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Kaman K-1200-1
|
|
gptkbp:influenced
|
later_Kaman_helicopters
|
|
gptkbp:legacy
|
influenced future helicopter designs.
|
|
gptkbp:length
|
40 ft
|
|
gptkbp:maintenance
|
routine inspections required
|
|
gptkbp:manufacturer
|
gptkb:Kaman_Aerospace_Corporation
|
|
gptkbp:maxSpeed
|
120 knots
|
|
gptkbp:maxTakeoffWeight
|
4,500 lbs
|
|
gptkbp:notableFeature
|
none reported
|
|
gptkbp:operationalHistory
|
used in various military operations
|
|
gptkbp:operationalRange
|
varied by load
|
|
gptkbp:participatesIn
|
transport and utility
|
|
gptkbp:passengerCapacity
|
2
|
|
gptkbp:primaryUser
|
gptkb:U.S._Army
|
|
gptkbp:productionCompany
|
1950s
|
|
gptkbp:productionYears
|
1960-1970
|
|
gptkbp:propulsion
|
turbine engine
|
|
gptkbp:range
|
300 nautical miles
|
|
gptkbp:relatedModel
|
gptkb:Kaman_K-1200-2
|
|
gptkbp:retirementYear
|
1980
|
|
gptkbp:role
|
utility helicopter
|
|
gptkbp:safetyFeatures
|
dual control system
|
|
gptkbp:service_ceiling
|
15,000 ft
|
|
gptkbp:services
|
1961
|
|
gptkbp:successor
|
gptkb:Kaman_K-1200-3
|
|
gptkbp:technology
|
varied by model
|
|
gptkbp:totalGoals
|
200 units
|
|
gptkbp:training
|
pilot training required
|
|
gptkbp:usedBy
|
gptkb:United_States_military
|
|
gptkbp:variant
|
K-1200-2
|
|
gptkbp:weight
|
2,500 lbs
|
|
gptkbp:wingspan
|
nan
|