Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:diameter |
0.34 m
|
| gptkbp:engine |
dual-thrust solid-fuel rocket
|
| gptkbp:enteredService |
1967
|
| gptkbp:fullName |
gptkb:RIM-66_Standard_MR
|
| gptkbp:guidanceSystem |
semi-active radar homing
|
| http://www.w3.org/2000/01/rdf-schema#label |
SM-1 missile
|
| gptkbp:length |
4.47 m
|
| gptkbp:manufacturer |
gptkb:Raytheon
|
| gptkbp:NATOReportingName |
Standard MR
|
| gptkbp:origin |
gptkb:United_States
|
| gptkbp:platform |
gptkb:ship
|
| gptkbp:predecessor |
gptkb:RIM-24_Tartar
|
| gptkbp:propulsion |
solid fuel
|
| gptkbp:range |
46 km
|
| gptkbp:speed |
Mach 3
|
| gptkbp:successor |
gptkb:SM-2_missile
|
| gptkbp:usedBy |
gptkb:United_States_Navy
gptkb:French_Navy gptkb:Royal_Australian_Navy gptkb:Spanish_Navy gptkb:Italian_Navy |
| gptkbp:warheadType |
62 kg
blast-fragmentation |
| gptkbp:weight |
617 kg
|
| gptkbp:bfsParent |
gptkb:SM-2_missiles
gptkb:SM-2_Block_IIIA/B_missiles |
| gptkbp:bfsLayer |
8
|