|
gptkbp:instanceOf
|
gptkb:helicopter
|
|
gptkbp:aircraft
|
200 miles
experimental aircraft
|
|
gptkbp:armament
|
none
|
|
gptkbp:controls
|
elevators
fly-by-wire
ailerons
rudder
|
|
gptkbp:crew
|
none
|
|
gptkbp:decommissioned
|
1960
|
|
gptkbp:design
|
ducted fan
autogyro
Henry_H._Hiller
|
|
gptkbp:enginePower
|
300 hp
|
|
gptkbp:engineType
|
turbine engine
|
|
gptkbp:firstFlight
|
1954
|
|
gptkbp:fuelCapacity
|
100 gallons
|
|
gptkbp:hasArea
|
gptkb:Robert_H._Hiller
|
|
gptkbp:headlights
|
yes
|
|
gptkbp:height
|
6 ft
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Hiller VZ-1 Pawnee
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
20 ft
|
|
gptkbp:manufacturer
|
gptkb:Hiller_Aircraft_Company
|
|
gptkbp:maxSpeed
|
100 mph
|
|
gptkbp:maxTakeoffWeight
|
1,500 lbs
1,800 lbs
|
|
gptkbp:missions
|
remote control
|
|
gptkbp:notableFeature
|
lightweight design
high maneuverability
vertical takeoff and landing
remote operation
low cost of production
|
|
gptkbp:numberBuilt
|
10
|
|
gptkbp:operationalArea
|
military training
|
|
gptkbp:productionYears
|
1954-1956
|
|
gptkbp:propulsion
|
single rotor
|
|
gptkbp:purpose
|
target drone
|
|
gptkbp:range
|
100 miles
|
|
gptkbp:relatedAircraft
|
gptkb:Hiller_OH-23_Raven
gptkb:Hiller_UH-12
Hiller_VZ-1
|
|
gptkbp:role
|
unmanned aerial vehicle
|
|
gptkbp:service_ceiling
|
10,000 ft
|
|
gptkbp:services
|
10,000 ft
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
none
|
|
gptkbp:usedBy
|
gptkb:United_States_Army
|
|
gptkbp:weight
|
1,200 lbs
|
|
gptkbp:wingspan
|
18 ft
|