Trident II D5 guidance system
GPTKB entity
Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
precision-guided munition
|
| gptkbp:accuracy |
less than 90 meters CEP
|
| gptkbp:component |
gptkb:Trident_II_D5_SLBM
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:enteredService |
1990s
|
| gptkbp:features |
onboard computer
inertial navigation system stellar sensor |
| gptkbp:guidanceSystem |
gptkb:Trident_II_D5_missile
astro-inertial |
| https://www.w3.org/2000/01/rdf-schema#label |
Trident II D5 guidance system
|
| gptkbp:manufacturer |
gptkb:Lockheed_Martin
gptkb:Charles_Stark_Draper_Laboratory |
| gptkbp:purpose |
nuclear deterrence
precision targeting |
| gptkbp:supports |
multiple independently targetable reentry vehicles (MIRVs)
|
| gptkbp:usedBy |
gptkb:Royal_Navy
gptkb:U.S._Navy gptkb:Trident_II_D5 |
| gptkbp:bfsParent |
gptkb:GPS_(Trident_II_D5)
|
| gptkbp:bfsLayer |
6
|