Statements (54)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:rocket
|
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:USS_America
|
| gptkbp:countermeasures |
limited effectiveness against advanced countermeasures
|
| gptkbp:deployment |
gptkb:starship
deployed on various classes of ships |
| gptkbp:developed_by |
gptkb:Raytheon
|
| gptkbp:developer |
developed over several decades
|
| gptkbp:diameter |
0.34 meters
|
| gptkbp:enemy |
high-explosive
|
| gptkbp:exported_to |
several allied nations
|
| gptkbp:features |
aerodynamic design for high speed
|
| gptkbp:fighting_style |
gptkb:Gulf_War
gptkb:battle |
| gptkbp:filmography |
gptkb:battle
|
| gptkbp:first_introduced |
1960s
|
| gptkbp:guidance_system |
semi-active radar homing
|
| gptkbp:has_ability |
gptkb:1970
|
| gptkbp:has_programs |
part of the Standard missile family
|
| gptkbp:historical_significance |
significant role in Cold War naval strategy
|
| https://www.w3.org/2000/01/rdf-schema#label |
RIM-66 Standard missile
|
| gptkbp:integrates_with |
integrated with Aegis radar system
|
| gptkbp:is_integrated_with |
interoperable with NATO systems
part of multi-layered defense system |
| gptkbp:is_tested_for |
extensive testing program conducted
|
| gptkbp:is_used_by |
gptkb:battle
|
| gptkbp:key |
high speed, long range, precision targeting
|
| gptkbp:launch_site |
gptkb:rocket
automated launch control systems |
| gptkbp:launch_vehicle |
ship-based launchers
|
| gptkbp:launched |
vertical launch system
|
| gptkbp:length |
3.66 meters
|
| gptkbp:market |
approximately $1 million
|
| gptkbp:membership |
SM-1
|
| gptkbp:military_branch |
primarily used by naval forces
|
| gptkbp:modifications |
upgraded guidance systems
|
| gptkbp:operational_range |
up to 100 km
|
| gptkbp:operational_status |
currently operational in several navies
|
| gptkbp:primary_user |
Japan, South Korea, Taiwan
|
| gptkbp:produced_by |
in service
|
| gptkbp:range |
up to 100 km
|
| gptkbp:reliability |
high
|
| gptkbp:service_history |
1960s to present
|
| gptkbp:speed |
Mach 2.5
|
| gptkbp:succeeded_by |
high success rate in tests
|
| gptkbp:successor |
gptkb:RIM-161_Standard_Missile_3
|
| gptkbp:targets |
aircraft, cruise missiles
|
| gptkbp:training |
conducted regularly
simulator training available |
| gptkbp:type |
gptkb:rocket
|
| gptkbp:upgrades |
planned future upgrades to enhance capabilities
ongoing upgrades to maintain effectiveness |
| gptkbp:variant |
RIM-66 A, RIM-66 B, RIM-66 C
|
| gptkbp:weight |
300 kg
|