Properties (50)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
rocket
|
| gptkbp:budget |
estimated $100 million
|
| gptkbp:collaboratesWith |
gptkb:Department_of_Defense
NASA |
| gptkbp:designedBy |
ULA_engineering_team
|
| gptkbp:designedFor |
commercial and government missions
|
| gptkbp:developer |
ongoing
|
| gptkbp:diameter |
5.4 meters
|
| gptkbp:engine |
BE-4
|
| gptkbp:features |
autonomous flight safety system
|
| gptkbp:firstAwarded |
gptkb:Centaur
|
| gptkbp:firstFlight |
2023
|
| gptkbp:firstMatch |
gptkb:Centaur_upper_stage
|
| gptkbp:has |
advanced avionics
multiple configurations |
| gptkbp:height |
60 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
Vulcan Centaur rocket
|
| gptkbp:is |
cost-effective
innovative environmentally friendly versatile reliable heavy-lift rocket a key player in space exploration a significant advancement in rocketry. designed for future missions expected to launch frequently next-generation rocket part_of_ULA's_strategy |
| gptkbp:launched |
frequent
|
| gptkbp:launchSite |
gptkb:Vandenberg_Space_Force_Base
gptkb:Cape_Canaveral_Space_Force_Station |
| gptkbp:manufacturer |
gptkb:United_Launch_Alliance
|
| gptkbp:mission |
satellite launch
|
| gptkbp:number_of_stages |
2
|
| gptkbp:partOf |
Vulcan_program
|
| gptkbp:passenger_traffic |
5.4 meters
|
| gptkbp:payloadCapacity |
6,500 kg
27,200 kg |
| gptkbp:reliability |
high
|
| gptkbp:replacedBy |
Atlas V
|
| gptkbp:setting |
dual-engine
|
| gptkbp:suitableFor |
interplanetary missions
|
| gptkbp:supports |
commercial satellite launches
scientific missions national security missions |
| gptkbp:targets |
2023
|
| gptkbp:uses |
reusable components
liquid oxygen and liquefied natural gas |
| gptkbp:usesTechnology |
Atlas V
|