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gptkbp:instanceOf
|
gptkb:helicopter
|
|
gptkbp:application
|
Hydraulic launcher
|
|
gptkbp:countryOfOrigin
|
gptkb:India
|
|
gptkbp:cruiseSpeed
|
125 km/h
|
|
gptkbp:developedBy
|
gptkb:Defence_Research_and_Development_Organisation
|
|
gptkbp:endurance
|
4 hours
|
|
gptkbp:engineType
|
gptkb:Wankel_rotary_engine
|
|
gptkbp:enteredService
|
2011
|
|
gptkbp:firstFlight
|
1995
|
|
gptkbp:length
|
4.63 m
|
|
gptkbp:manufacturer
|
gptkb:Aeronautical_Development_Establishment
|
|
gptkbp:maximumSpeed
|
185 km/h
|
|
gptkbp:maxTakeoffWeight
|
380 kg
|
|
gptkbp:numberBuilt
|
14
|
|
gptkbp:operationalCeiling
|
3,600 m
|
|
gptkbp:payload
|
CCD camera
Electro-optic sensors
Laser range finder
Thermal imager
|
|
gptkbp:range
|
160 km
|
|
gptkbp:recoveryMethod
|
Parachute
|
|
gptkbp:retired
|
2016
|
|
gptkbp:role
|
gptkb:Surveillance
Reconnaissance
Target acquisition
Artillery fire correction
|
|
gptkbp:status
|
Retired
|
|
gptkbp:usedBy
|
Indian Army
|
|
gptkbp:wingspan
|
6.57 m
|
|
gptkbp:bfsParent
|
gptkb:Aeronautical_Development_Establishment_(ADE)
|
|
gptkbp:bfsLayer
|
7
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Nishant UAV
|