Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:marine
|
| gptkbp:alternativeName |
gptkb:Trident_D5
|
| gptkbp:awardedContract |
1983
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
2.11 m
|
| gptkbp:enteredService |
1990
|
| gptkbp:guidanceSystem |
gptkb:GPS
astro-inertial guidance |
| https://www.w3.org/2000/01/rdf-schema#label |
UGM-133 Trident II
|
| gptkbp:introduced |
1990
|
| gptkbp:length |
13.42 m
|
| gptkbp:manufacturer |
gptkb:Lockheed_Martin_Space_Systems
|
| gptkbp:numberOfStages |
3
|
| gptkbp:payload |
up to 12 warheads
|
| gptkbp:platform |
gptkb:marine
|
| gptkbp:predecessor |
gptkb:UGM-96_Trident_I
|
| gptkbp:propulsion |
solid fuel
|
| gptkbp:range |
over 7,800 km
|
| gptkbp:speed |
over Mach 24
|
| gptkbp:status |
in service
|
| gptkbp:testLaunches |
over 170 successful
|
| gptkbp:usedBy |
gptkb:Royal_Navy
gptkb:United_States_Navy |
| gptkbp:warheadType |
MIRV nuclear warheads
|
| gptkbp:weight |
58,500 kg
|
| gptkbp:bfsParent |
gptkb:UGM-96
gptkb:UGM-96_Trident_I |
| gptkbp:bfsLayer |
7
|