Vulcan Spacecraft

GPTKB entity

Statements (52)
Predicate Object
gptkbp:instance_of gptkb:spacecraft
gptkbp:advances new propulsion systems
gptkbp:challenges complex integration
gptkbp:collaboration gptkb:NASA
various space agencies
gptkbp:configuration two-stage
gptkbp:control_system digital fly-by-wire
gptkbp:debut upcoming missions planned.
gptkbp:debut_year gptkb:2023
gptkbp:design_purpose heavy-lift missions
gptkbp:development_cost $1 billion
gptkbp:durability partial
gptkbp:engine gptkb:Blue_Origin
gptkbp:engine_type gptkb:BE-4
gptkbp:first_flight gptkb:2023
planned before operational use
gptkbp:fuel_type liquid natural gas
gptkbp:future_plans expand capabilities
gptkbp:guidance_system gptkb:navigation_system
gptkbp:height 60 meters
https://www.w3.org/2000/01/rdf-schema#label Vulcan Spacecraft
gptkbp:involved_technology advanced avionics
gptkbp:key_feature high reliability
gptkbp:launch_date up to 12 launches per year
gptkbp:launch_platform gptkb:United_Launch_Alliance
gptkbp:launch_price $100 million
gptkbp:launch_site gptkb:Cape_Canaveral_Space_Force_Station
gptkbp:launch_vehicle gptkb:Vulcan_Centaur
gptkbp:launch_window specific mission requirements
gptkbp:launched single or dual payloads
gptkbp:manufacturer gptkb:United_Launch_Alliance
gptkbp:market_segment government and commercial
gptkbp:mission orbital insertion
Lunar lander mission
gptkbp:mission_duration varies by mission
gptkbp:operational_status in development
gptkbp:orbit_type Low Earth Orbit (LEO)
gptkbp:part_of United Launch Alliance fleet
gptkbp:payload_capacity modular design
5.4 meters
up to 27,200 kg to LEO
satellites, interplanetary missions
gptkbp:project ongoing development
gptkbp:propulsion 2,400 k N
gptkbp:public_interest high
gptkbp:replaces gptkb:Atlas_V
gptkbp:safety_measures rigorous testing required
gptkbp:safety_rating high
gptkbp:sustainability_features lower emissions
gptkbp:target_market commercial satellite launches
gptkbp:bfsParent gptkb:Ferengi
gptkbp:bfsLayer 5