|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:collaborates_with
|
gptkb:Lockheed_Martin
gptkb:Northrop_Grumman
gptkb:Boeing
gptkb:Blue_Origin
|
|
gptkbp:configuration
|
Vulcan 1
Vulcan 2
|
|
gptkbp:design_features
|
flexibility
scalability
cost efficiency
high reliability
|
|
gptkbp:designed_for
|
satellite launches
deep space missions
heavy payloads
|
|
gptkbp:development_cost
|
$1 billion
|
|
gptkbp:diameter
|
5.4 meters
|
|
gptkbp:engine
|
gptkb:BE-4
|
|
gptkbp:expected_operational_date
|
2024
|
|
gptkbp:first_flight
|
gptkb:2023
|
|
gptkbp:height
|
60 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
ULA Vulcan Centaur
|
|
gptkbp:is_integrated_with
|
ULA's Vertical Integration Facility
|
|
gptkbp:launch_date
|
up to 12 per year
|
|
gptkbp:launch_platform
|
gptkb:United_Launch_Alliance
ULA's Launch Control Center
|
|
gptkbp:launch_price
|
estimated $100 million
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
gptkb:Cape_Canaveral_Space_Force_Station
|
|
gptkbp:launch_vehicle
|
Vulcan family
|
|
gptkbp:manufacturer
|
gptkb:United_Launch_Alliance
|
|
gptkbp:mission_type
|
gptkb:government
commercial
scientific
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:operational_status
|
in development
|
|
gptkbp:part_of
|
gptkb:NASA's_Artemis_program
gptkb:National_Security_Space_Launch_program
|
|
gptkbp:payload_capacity
|
gptkb:Psyche_spacecraft
6,500 kg
27,200 kg
5.4 m diameter
Lunar Gateway components
|
|
gptkbp:reliability
|
high
|
|
gptkbp:replaces
|
gptkb:Delta_IV
gptkb:Atlas_V
|
|
gptkbp:successor
|
gptkb:Delta_IV
gptkb:Atlas_V
|
|
gptkbp:target_market
|
government agencies
scientific organizations
international customers
commercial satellite operators
|
|
gptkbp:transportation
|
gptkb:railway
road transport
mobile launcher
|
|
gptkbp:uses
|
modular design
advanced materials
reusable technology
digital engineering
|
|
gptkbp:bfsParent
|
gptkb:Aerojet_Rocketdyne's_AR1
|
|
gptkbp:bfsLayer
|
6
|