|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Titan_rocket
|
|
gptkbp:associated_with
|
U. S. military history
|
|
gptkbp:contract
|
gptkb:1955
|
|
gptkbp:controls
|
gptkb:auto_race
|
|
gptkbp:country
|
gptkb:United_States
|
|
gptkbp:debut_year
|
1964-02-16
1965-04-24
|
|
gptkbp:decommissioned
|
gptkb:1965
|
|
gptkbp:deployment
|
gptkb:1964
gptkb:1965
|
|
gptkbp:design
|
nuclear deterrence
two-stage rocket
|
|
gptkbp:designated_as
|
SM-68
|
|
gptkbp:developed_by
|
gptkb:aircraft
|
|
gptkbp:developer
|
1955-1964
|
|
gptkbp:diameter
|
3.05 meters
|
|
gptkbp:enemy
|
gptkb:weapon
|
|
gptkbp:engine
|
2
L R87
|
|
gptkbp:engine_type
|
gptkb:rocket
L R87
|
|
gptkbp:first_flight
|
gptkb:3
1964-02-16
1965-04-24
1963-12-06
1959-02-06
|
|
gptkbp:frequency
|
1964-1965
|
|
gptkbp:fuel_type
|
gptkb:RP-1_kerosene
RP-1 and liquid oxygen
|
|
gptkbp:guidance_system
|
1,500 meters
inertial guidance system
|
|
gptkbp:height
|
30.5 meters
|
|
gptkbp:historical_significance
|
early ICBM development
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Titan I
|
|
gptkbp:influenced
|
gptkb:Titan_II
|
|
gptkbp:influenced_by
|
gptkb:Redstone_rocket
|
|
gptkbp:inspired
|
later ICB Ms
|
|
gptkbp:is_used_by
|
gptkb:aircraft
|
|
gptkbp:is_used_for
|
gptkb:military_unit
|
|
gptkbp:launch_date
|
1965-01-01
|
|
gptkbp:launch_site
|
gptkb:cape
gptkb:Cape_Canaveral_Air_Force_Station
gptkb:railway_station
mobile launch platform
ground launch
|
|
gptkbp:launch_vehicle
|
gptkb:planet
gptkb:rocket
gptkb:Launch_Complex_16
140,000 kg
military launch vehicle
|
|
gptkbp:launched
|
gptkb:10
gptkb:12
gptkb:Complex_16
1960-01-01
|
|
gptkbp:length
|
30.5 meters
|
|
gptkbp:manufacturer
|
gptkb:Martin_Company
gptkb:Martin_Marietta
|
|
gptkbp:market
|
$1 million
|
|
gptkbp:max_speed
|
24,000 km/h
|
|
gptkbp:military_branch
|
gptkb:aircraft
|
|
gptkbp:notable_feature
|
gptkb:first_U._S._ICBM
|
|
gptkbp:number_built
|
gptkb:12
|
|
gptkbp:number_of_stages
|
gptkb:Titan_I_first_stage
gptkb:Titan_I_second_stage
2
|
|
gptkbp:operated_by
|
gptkb:aircraft
|
|
gptkbp:operational_area
|
gptkb:1965
gptkb:Monarch
1959-1965
nuclear deterrence
|
|
gptkbp:operational_status
|
decommissioned
|
|
gptkbp:origin
|
gptkb:United_States
|
|
gptkbp:produced_by
|
gptkb:10
|
|
gptkbp:propulsion
|
150,000 lbf
RP-1 and liquid oxygen
1500 k N
|
|
gptkbp:range
|
10,000 km
|
|
gptkbp:related_to
|
gptkb:Titan_family_of_rockets
|
|
gptkbp:retired
|
gptkb:1965
|
|
gptkbp:retirement_year
|
gptkb:1965
superseded by Titan II
|
|
gptkbp:role
|
gptkb:rocket
strategic missile
|
|
gptkbp:seating_capacity
|
3,000 kg
|
|
gptkbp:social_structure
|
liquid oxygen
|
|
gptkbp:status
|
retired
|
|
gptkbp:succeeded_by
|
100%
|
|
gptkbp:successor
|
gptkb:Titan_II_program
gptkb:Titan_II
gptkb:CEO
|
|
gptkbp:used_in
|
gptkb:Monarch
|
|
gptkbp:wingspan
|
0 meters
|