|
gptkbp:instance_of
|
gptkb:software
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Titan_I
|
|
gptkbp:associated_with
|
gptkb:Monarch
|
|
gptkbp:base
|
various U. S. Air Force bases
|
|
gptkbp:controls
|
computerized control system
|
|
gptkbp:country
|
gptkb:none
|
|
gptkbp:decommissioned
|
gptkb:1987
|
|
gptkbp:defense
|
U. S. nuclear deterrent strategy
|
|
gptkbp:developed_by
|
gptkb:aircraft
|
|
gptkbp:developer
|
gptkb:1955
gptkb:1962
|
|
gptkbp:diameter
|
10 feet
|
|
gptkbp:engine
|
2
|
|
gptkbp:engine_type
|
liquid-fueled
|
|
gptkbp:events
|
high
|
|
gptkbp:first_flight
|
gptkb:1962
gptkb:1987
successful
|
|
gptkbp:fuel_type
|
RP-1 and liquid oxygen
|
|
gptkbp:guidance_system
|
inertial guidance
|
|
gptkbp:has_ability
|
gptkb:1963
|
|
gptkbp:height
|
103 feet
|
|
gptkbp:historical_impact
|
significant during the Cold War
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Titan II program
|
|
gptkbp:influenced_by
|
gptkb:NASA's_Gemini_program
|
|
gptkbp:is_influenced_by
|
rocket propulsion technology
|
|
gptkbp:is_tested_for
|
multiple successful test launches
|
|
gptkbp:is_used_for
|
military purposes
|
|
gptkbp:launch_date
|
gptkb:1987
approximately once a month
|
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral_Air_Force_Station
ground-based
underground silos
underground launch control center
|
|
gptkbp:launch_vehicle
|
gptkb:Titan_II
gptkb:CEO
|
|
gptkbp:launched
|
gptkb:39
varied by mission
Complex 40
|
|
gptkbp:legacy
|
paved the way for future ICB Ms
|
|
gptkbp:manufacturer
|
gptkb:Martin_Marietta
|
|
gptkbp:military_branch
|
gptkb:aircraft
|
|
gptkbp:mission
|
gptkb:rocket
|
|
gptkbp:notable_album
|
first successful launch in 1962
|
|
gptkbp:notable_feature
|
two-stage rocket
|
|
gptkbp:operational_area
|
gptkb:aircraft
deterrence
1962-1987
|
|
gptkbp:operational_status
|
retired from service
|
|
gptkbp:price
|
$1.5 billion
|
|
gptkbp:project
|
gptkb:Project_Gemini
|
|
gptkbp:propulsion
|
430,000 pounds
|
|
gptkbp:related_to
|
gptkb:Titan_I
|
|
gptkbp:replaced_by
|
gptkb:Minuteman_missile
|
|
gptkbp:retirement_year
|
gptkb:1987
|
|
gptkbp:seating_capacity
|
up to 16,000 pounds
|
|
gptkbp:significance
|
first ICBM with a high payload capacity
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Titan_III
|
|
gptkbp:technology
|
ballistic missile technology
|
|
gptkbp:used_in
|
gptkb:battle
|