gptkbp:instance_of
|
gptkb:rocket
|
gptkbp:bfsLayer
|
4
|
gptkbp:bfsParent
|
gptkb:Atlas_rocket
|
gptkbp:associated_with
|
gptkb:U._S._Space_Program
|
gptkbp:controls
|
gptkb:Autopilot
|
gptkbp:deployment
|
gptkb:1959
gptkb:1965
Silo and mobile
|
gptkbp:designed_by
|
gptkb:Convair
|
gptkbp:developed_by
|
gptkb:aircraft
|
gptkbp:developer
|
5 years
|
gptkbp:diameter
|
3.05 meters
|
gptkbp:enemy
|
gptkb:Nuclear_warhead
|
gptkbp:engine_type
|
gptkb:rocket
|
gptkbp:features
|
Two-stage design
|
gptkbp:first_flight
|
gptkb:1956
gptkb:1965
Over 50
|
gptkbp:fuel_type
|
RP-1 and Liquid Oxygen
|
gptkbp:guidance_system
|
Inertial guidance
|
gptkbp:has_programs
|
gptkb:Project_Mercury
|
gptkbp:historical_context
|
Nuclear deterrence strategy
|
https://www.w3.org/2000/01/rdf-schema#label
|
Atlas D
|
gptkbp:influenced_by
|
Vanguard program
|
gptkbp:inspired_by
|
gptkb:German_V-2_rocket
|
gptkbp:is_influential_in
|
Subsequent ICB Ms
|
gptkbp:is_used_by
|
gptkb:aircraft
|
gptkbp:launch_site
|
gptkb:cape
Ground launch
Mobile launch platform
|
gptkbp:legacy
|
Foundation for future missile technology
|
gptkbp:length
|
30.5 meters
|
gptkbp:manufacturer
|
gptkb:Convair
|
gptkbp:market
|
$18 million
|
gptkbp:max_takeoff_weight
|
130,000 kg
|
gptkbp:notable_album
|
First successful launch in 1958
|
gptkbp:notable_users
|
gptkb:U._S._military
|
gptkbp:number_built
|
more than 100
|
gptkbp:number_of_stages
|
2
|
gptkbp:operational_area
|
gptkb:1959
1959-1965
Strategic deterrent
|
gptkbp:operational_range
|
5,500 km
|
gptkbp:operational_status
|
Retired
|
gptkbp:origin
|
gptkb:United_States
|
gptkbp:related_to
|
gptkb:Monarch
|
gptkbp:reliability
|
gptkb:High
|
gptkbp:retired
|
gptkb:1965
|
gptkbp:retirement_year
|
Obsolescence
|
gptkbp:role
|
gptkb:rocket
|
gptkbp:seating_capacity
|
1,500 kg to Low Earth Orbit
|
gptkbp:significance
|
gptkb:First_U._S._ICBM
|
gptkbp:status
|
Retired
|
gptkbp:successor
|
gptkb:Atlas_E
gptkb:Project_Atlas
|
gptkbp:used_in
|
Early space missions
|