|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:configuration
|
gptkb:Vulcan_501
Vulcan 401
|
|
gptkbp:debut
|
gptkb:2023
|
|
gptkbp:development
|
gptkb:true
|
|
gptkbp:development_cost
|
estimated $1 billion
|
|
gptkbp:diameter
|
5.4 meters
|
|
gptkbp:engine
|
gptkb:Blue_Origin
|
|
gptkbp:engine_type
|
gptkb:BE-4
|
|
gptkbp:environmental_impact
|
minimized
|
|
gptkbp:first_flight
|
gptkb:2023
planned
|
|
gptkbp:future_plans
|
gptkb:Mars_missions
Lunar missions
deep space missions
|
|
gptkbp:guidance_system
|
gptkb:navigation_system
|
|
gptkbp:height
|
60 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Vulcan Centaur
|
|
gptkbp:launch_date
|
up to 12 launches per year
|
|
gptkbp:launch_event
|
targeting 98%
|
|
gptkbp:launch_platform
|
gptkb:ground
gptkb:United_Launch_Alliance
|
|
gptkbp:launch_price
|
estimated $100 million
|
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral_Space_Force_Station
|
|
gptkbp:launch_vehicle
|
gptkb:Vulcan
optional
|
|
gptkbp:launch_window
|
varies by mission
|
|
gptkbp:lifespan
|
20 years
|
|
gptkbp:manufacturer
|
gptkb:United_Launch_Alliance
|
|
gptkbp:mission
|
vertical launch
|
|
gptkbp:notable_mission
|
gptkb:Artemis_program
|
|
gptkbp:number_of_stages
|
gptkb:Centaur
2
|
|
gptkbp:partnerships
|
gptkb:NASA
commercial partners
|
|
gptkbp:payload_capacity
|
5.4 meters
27,200 kg
up to 27,000 kg to LEO
6,700 kg
ULA facilities
|
|
gptkbp:production_status
|
in development
|
|
gptkbp:regulatory_compliance
|
required
|
|
gptkbp:release_country
|
possible
|
|
gptkbp:reliability
|
high
|
|
gptkbp:replaces
|
gptkb:Atlas_V
|
|
gptkbp:safety_record
|
excellent
|
|
gptkbp:target_market
|
commercial satellite launches
interplanetary missions
government satellite launches
|
|
gptkbp:technology
|
advanced avionics
high-performance engines
reusable components
|
|
gptkbp:uses
|
Centaur upper stage
|
|
gptkbp:uses_rocket_engine
|
gptkb:BE-4
|
|
gptkbp:bfsParent
|
gptkb:NASA_Stennis_Space_Center
gptkb:United_Launch_Alliance
|
|
gptkbp:bfsLayer
|
4
|