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gptkbp:instanceOf
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gptkb:spacecraft
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|
gptkbp:developedBy
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gptkb:Lockheed_Martin
gptkb:Raytheon
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gptkbp:diameter
|
127 mm
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gptkbp:environmentalImpact
|
Waterproof
Temperature resistant
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gptkbp:firstMatch
|
1992
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|
https://www.w3.org/2000/01/rdf-schema#label
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Javelin missile
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gptkbp:introduced
|
1996
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gptkbp:launched
|
15 to 45 degrees
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gptkbp:launchSite
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gptkb:Command_Launch_Unit_(CLU)
Shoulder-fired
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|
gptkbp:length
|
1.2 m
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|
gptkbp:maxSpeed
|
200 m/s
|
|
gptkbp:maxTakeoffWeight
|
49.6 kg with CLU
|
|
gptkbp:notable_player
|
Single shot
Salvo
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|
gptkbp:offers
|
$80,000
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gptkbp:operationalRange
|
2.5 km
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|
gptkbp:operationalStatus
|
In service
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gptkbp:primaryUser
|
gptkb:Jordanian_Armed_Forces
gptkb:British_Army
gptkb:Canadian_Armed_Forces
gptkb:UAE_Armed_Forces
gptkb:United_States_Army
gptkb:Indian_Armed_Forces
gptkb:Australian_Army
gptkb:Philippine_Army
gptkb:United_States_Marine_Corps
gptkb:Taiwanese_Armed_Forces
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|
gptkbp:productionCompany
|
1983
|
|
gptkbp:productionStartYear
|
1994
|
|
gptkbp:propulsion
|
Solid-fuel rocket motor
|
|
gptkbp:provides
|
Automatic target tracking
Fire-and-forget
Infrared_homing
|
|
gptkbp:range
|
2.5 km
|
|
gptkbp:refreshRate
|
30 seconds
|
|
gptkbp:relatedPatent
|
gptkb:TOW_missile
FGM-148 Javelin
|
|
gptkbp:safetyFeatures
|
Self-destruct mechanism
Arming delay
Launch lock
Launch safety system
|
|
gptkbp:sensors
|
Inertial navigation system
Laser rangefinder
Infrared seeker
|
|
gptkbp:successor
|
nan
|
|
gptkbp:supportRole
|
gptkb:Gulf_War
gptkb:Russo-Ukrainian_War
gptkb:Syrian_Civil_War
gptkb:Iraq_War
War_in_Afghanistan
|
|
gptkbp:targets
|
Direct attack
Top attack
|
|
gptkbp:training
|
Simulator training available
|
|
gptkbp:type
|
gptkb:Tandem_HEAT
|
|
gptkbp:weight
|
22.3 kg
|