|
gptkbp:instanceOf
|
gptkb:surface-to-air_missile
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:diameter
|
0.34 m
|
|
gptkbp:enteredService
|
1998
|
|
gptkbp:guidanceSystem
|
inertial guidance
semi-active radar homing
|
|
gptkbp:improves
|
enhanced maneuverability
improved proximity fuze
improved warhead
|
|
gptkbp:length
|
4.72 m
|
|
gptkbp:manufacturer
|
gptkb:Raytheon
|
|
gptkbp:partOf
|
gptkb:Standard_Missile_family
|
|
gptkbp:platform
|
gptkb:Mk_41_Vertical_Launching_System
gptkb:Aegis_Combat_System
|
|
gptkbp:predecessor
|
gptkb:SM-2_Block_III
|
|
gptkbp:purpose
|
anti-air warfare
fleet area air defense
|
|
gptkbp:range
|
167 km
|
|
gptkbp:speed
|
Mach 3.5
|
|
gptkbp:successor
|
gptkb:SM-2_Block_IIIB
|
|
gptkbp:usedBy
|
gptkb:United_States_Navy
gptkb:Japan_Maritime_Self-Defense_Force
gptkb:Royal_Australian_Navy
gptkb:German_Navy
gptkb:Republic_of_Korea_Navy
gptkb:Royal_Netherlands_Navy
gptkb:Spanish_Navy
|
|
gptkbp:warheadType
|
blast-fragmentation
|
|
gptkbp:weight
|
707 kg
|
|
gptkbp:bfsParent
|
gptkb:SM2
|
|
gptkbp:bfsLayer
|
7
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
SM-2 Block IIIA
|