|
gptkbp:instanceOf
|
rocket
|
|
gptkbp:cultural_heritage
|
Atlas_and_Delta_rockets
|
|
gptkbp:design
|
modular
|
|
gptkbp:developer
|
estimated $1 billion
|
|
gptkbp:diameter
|
5.4 meters
|
|
gptkbp:engine
|
BE-4
|
|
gptkbp:engineType
|
solid
liquid
|
|
gptkbp:environmentalImpact
|
minimized emissions
|
|
gptkbp:firstAwarded
|
gptkb:Centaur_upper_stage
4
|
|
gptkbp:firstFlight
|
2023
planned
static fire tests
simulations conducted
|
|
gptkbp:futurePlans
|
advanced avionics
new engines
enhanced payload capacity
|
|
gptkbp:hasGoals
|
2
|
|
gptkbp:height
|
60 meters
|
|
gptkbp:highestPoint
|
1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Vulcan Centaur
|
|
gptkbp:internationalCooperation
|
yes
launches for foreign customers
|
|
gptkbp:isDiscussedIn
|
gptkb:US_Department_of_Defense
NASA
commercial satellite operators
|
|
gptkbp:launched
|
competitive
remote monitoring
ground-based
up to 12 per year
|
|
gptkbp:launchSite
|
gptkb:Vandenberg_Space_Force_Base
gptkb:Cape_Canaveral_Space_Force_Station
|
|
gptkbp:manufacturer
|
gptkb:United_Launch_Alliance
|
|
gptkbp:missionCapabilities
|
GTO, LEO, SSO
|
|
gptkbp:missionsConducted
|
high
|
|
gptkbp:partnerships
|
gptkb:Lockheed_Martin
gptkb:Northrop_Grumman
Blue Origin
Aerojet Rocketdyne
|
|
gptkbp:passenger_traffic
|
5.4 meters
satellites, probes
|
|
gptkbp:payloadCapacity
|
27,200 kg
6,700 kg
|
|
gptkbp:productionCompany
|
in development
|
|
gptkbp:purpose
|
satellite launches
|
|
gptkbp:reliability
|
no
high
|
|
gptkbp:safetyFeatures
|
redundant systems
escape system
automated launch sequence
|
|
gptkbp:secondaryMission
|
interplanetary missions
lunar missions
Mars_missions
|
|
gptkbp:setting
|
two-stage
|
|
gptkbp:successor
|
Atlas V
|
|
gptkbp:targetMarket
|
commercial spaceflight
government missions
|