|
gptkbp:instance_of
|
gptkb:missile
|
|
gptkbp:debut
|
1975-01-01
1962-03-01
|
|
gptkbp:decommissioned
|
gptkb:1975
|
|
gptkbp:deployment
|
gptkb:1962
gptkb:1963
gptkb:United_States
|
|
gptkbp:design
|
gptkb:SM-65
1955-1960
|
|
gptkbp:development
|
1955-1962
|
|
gptkbp:diameter
|
3.05 meters
|
|
gptkbp:engine_type
|
gptkb:RD-180
|
|
gptkbp:first_flight
|
gptkb:1962
1975-01-01
|
|
gptkbp:fuel_type
|
RP-1 and liquid oxygen
|
|
gptkbp:guidance_system
|
1,500 meters
inertial
inertial guidance
|
|
gptkbp:has_programs
|
gptkb:Project_Atlas
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Atlas F
|
|
gptkbp:international_relations
|
yes
|
|
gptkbp:is_tested_for
|
multiple
suborbital
|
|
gptkbp:last_operational
|
gptkb:1975
|
|
gptkbp:launch_date
|
1962-03-01
|
|
gptkbp:launch_platform
|
ground launch
vertical launch
ground-based control
|
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral
|
|
gptkbp:launch_vehicle
|
gptkb:missile
|
|
gptkbp:launched
|
Complex 14
|
|
gptkbp:length
|
30.5 meters
|
|
gptkbp:manufacturer
|
gptkb:Convair
|
|
gptkbp:max_takeoff_weight
|
130,000 kg
|
|
gptkbp:military_branch
|
gptkb:United_States_Air_Force
|
|
gptkbp:military_technology
|
no
yes
|
|
gptkbp:number_built
|
gptkb:200
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:operational_period
|
1963-1975
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:operational_use
|
gptkb:1963
nuclear deterrence
|
|
gptkbp:payload_capacity
|
1,200 kg
|
|
gptkbp:propulsion
|
gptkb:liquid
500,000 lbf
|
|
gptkbp:range
|
gptkb:Vandenberg_Air_Force_Base
9,600 km
|
|
gptkbp:retired
|
gptkb:1975
|
|
gptkbp:retirement
|
replacement by more advanced systems
|
|
gptkbp:role
|
strategic deterrent
|
|
gptkbp:service_branch
|
gptkb:United_States_Air_Force
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Minuteman
gptkb:Titan_II
|
|
gptkbp:warhead_type
|
thermonuclear
|
|
gptkbp:bfsParent
|
gptkb:Space_Launch_Complex_15
gptkb:Atlas_rocket
gptkb:Launch_Complex_14
|
|
gptkbp:bfsLayer
|
5
|