Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
precision-guided munition
|
| gptkbp:accuracy |
less than 90 meters CEP
|
| gptkbp:component |
gptkb:Trident_II_missile
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:enables |
multiple independently targetable reentry vehicles (MIRVs)
|
| gptkbp:enteredService |
1990s
|
| gptkbp:features |
onboard computer
inertial navigation system stellar sensor |
| gptkbp:guidanceSystem |
astro-inertial guidance
|
| https://www.w3.org/2000/01/rdf-schema#label |
Trident II Guidance System
|
| gptkbp:manufacturer |
gptkb:Lockheed_Martin
gptkb:Charles_Stark_Draper_Laboratory |
| gptkbp:purpose |
gptkb:navigation
targeting |
| gptkbp:relatedTo |
gptkb:Polaris_missile_guidance_system
gptkb:Poseidon_missile_guidance_system |
| gptkbp:usedBy |
gptkb:Royal_Navy
gptkb:United_States_Navy gptkb:Trident_II_missile gptkb:UGM-133A_Trident_II |
| gptkbp:bfsParent |
gptkb:Draper_Laboratory
|
| gptkbp:bfsLayer |
5
|