Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:rocket
|
| gptkbp:country |
United Kingdom (as Trident II D5)
|
| gptkbp:developed_by |
gptkb:Lockheed_Martin
|
| gptkbp:diameter |
2.34 meters
|
| gptkbp:enemy |
gptkb:weapon
|
| gptkbp:first_flight |
successful
|
| gptkbp:first_introduced |
gptkb:1990
|
| gptkbp:guidance_system |
inertial guidance system
|
| https://www.w3.org/2000/01/rdf-schema#label |
Trident II missile
|
| gptkbp:is_used_by |
gptkb:battle
|
| gptkbp:launch_site |
gptkb:Ohio-class_submarine
submarine launched |
| gptkbp:length |
13.42 meters
|
| gptkbp:number_of_stages |
three
|
| gptkbp:operational_status |
in service
|
| gptkbp:propulsion |
solid propellant
|
| gptkbp:range |
over 7,000 miles
|
| gptkbp:reliability |
high reliability
|
| gptkbp:roll_rate |
part of the U. S. nuclear triad
|
| gptkbp:seating_capacity |
up to 8 warheads
|
| gptkbp:speed |
Mach 24
|
| gptkbp:stealth_features |
low radar cross-section
|
| gptkbp:strategic_importance |
deterrence
|
| gptkbp:successor |
gptkb:Trident_I_missile
|
| gptkbp:weight |
58,000 pounds
|
| gptkbp:bfsParent |
gptkb:Trident_engine
|
| gptkbp:bfsLayer |
5
|