|
gptkbp:instanceOf
|
gptkb:helicopter
|
|
gptkbp:armament
|
nan
|
|
gptkbp:communicationEquipment
|
Data link
|
|
gptkbp:controls
|
Remote control
|
|
gptkbp:design
|
gptkb:Iran
Reconnaissance and surveillance
|
|
gptkbp:designedBy
|
gptkb:Iran
|
|
gptkbp:developer
|
1980s to present
|
|
gptkbp:endurance
|
6 hours
|
|
gptkbp:enginePower
|
20 hp
|
|
gptkbp:engineType
|
gptkb:Piston_engine
|
|
gptkbp:exportedTo
|
No
|
|
gptkbp:firstFlight
|
1985
|
|
gptkbp:fuelType
|
Aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mohajer UAV
|
|
gptkbp:influencedBy
|
Western UAV designs
|
|
gptkbp:keyIssues
|
High altitude
Cost-effective
Long endurance
User-friendly operation
Field deployable
Versatile_payloads
|
|
gptkbp:landingGear
|
Tricycle
|
|
gptkbp:launchSite
|
gptkb:Catapult
|
|
gptkbp:length
|
2.5 meters
|
|
gptkbp:maxSpeed
|
200 km/h
|
|
gptkbp:maxTakeoffWeight
|
120 kg
|
|
gptkbp:militaryRank
|
gptkb:Iranian_Armed_Forces
No
|
|
gptkbp:modifications
|
Yes
|
|
gptkbp:navigationEquipment
|
gptkb:GPS
|
|
gptkbp:notableOperations
|
Surveillance missions
|
|
gptkbp:numberBuilt
|
Over 100
|
|
gptkbp:operationalRange
|
150 km
|
|
gptkbp:operationalStatus
|
Active
|
|
gptkbp:payloadCapacity
|
40 kg
|
|
gptkbp:photography
|
Electro-optical
|
|
gptkbp:primaryUser
|
gptkb:Islamic_Republic_of_Iran_Air_Force
|
|
gptkbp:productionCompany
|
In service
|
|
gptkbp:productionStartYear
|
1985
|
|
gptkbp:relatedTo
|
Mohajer-2
Mohajer-3
Mohajer-4
|
|
gptkbp:role
|
Reconnaissance
|
|
gptkbp:security
|
Limited
|
|
gptkbp:service_ceiling
|
5,000 meters
|
|
gptkbp:services
|
1985
|
|
gptkbp:successor
|
Mohajer-2
|
|
gptkbp:supportRole
|
Yes
|
|
gptkbp:usedBy
|
gptkb:Iranian_military
|
|
gptkbp:variant
|
Mohajer-2
Mohajer-3
Mohajer-4
|
|
gptkbp:weight
|
100 kg
|
|
gptkbp:wingspan
|
3.2 meters
|