Statements (60)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Team_Rocket
|
| gptkbp:academic_programs |
experienced engineering team
|
| gptkbp:advances |
new propulsion systems
|
| gptkbp:community_engagement |
community engagement initiatives planned
|
| gptkbp:community_outreach |
educational outreach programs planned
|
| gptkbp:control_system |
digital
|
| gptkbp:customer_support |
dedicated customer support team
|
| gptkbp:debut |
gptkb:2023
|
| gptkbp:design |
gptkb:Blue_Origin
|
| gptkbp:development_cost |
estimated $1 billion
|
| gptkbp:diameter |
5.4 meters
|
| gptkbp:durability |
partially reusable
|
| gptkbp:engine_type |
gptkb:BE-4
|
| gptkbp:environmental_impact |
designed to minimize emissions
|
| gptkbp:first_flight |
gptkb:2023
planned before operational use |
| gptkbp:fuel_type |
liquid oxygen and liquefied natural gas
|
| gptkbp:guidance_system |
inertial navigation
|
| gptkbp:height |
60 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
Vulcan Centaur 401
|
| gptkbp:integration |
shorter than previous models
|
| gptkbp:launch_date |
up to 12 launches per year
|
| gptkbp:launch_event |
major launch events planned
|
| gptkbp:launch_platform |
vertical launch
comprehensive post-launch analysis remote and ground control |
| gptkbp:launch_price |
$100 million
|
| gptkbp:launch_site |
gptkb:Cape_Canaveral_Space_Force_Station
|
| gptkbp:launch_vehicle |
gptkb:Vulcan
modern design principles |
| gptkbp:launch_window |
flexible launch windows
|
| gptkbp:launched |
streamlined launch preparation process
|
| gptkbp:manufacturer |
gptkb:United_Launch_Alliance
|
| gptkbp:media_coverage |
extensive media coverage expected
|
| gptkbp:mission |
high mission success rate expected
|
| gptkbp:mission_type |
commercial
|
| gptkbp:number_of_stages |
two
|
| gptkbp:operational_status |
in development
|
| gptkbp:orbital_altitude |
precise orbital insertion capabilities
|
| gptkbp:partnerships |
NASA, U. S. Department of Defense
|
| gptkbp:payload_capacity |
6,500 kg
5.4 meters 27,200 kg multiple payloads modular payload integration satellites, interplanetary missions |
| gptkbp:project |
on schedule for first launch
|
| gptkbp:propulsion |
1,000,000 lbf
|
| gptkbp:public_interest |
high public interest
|
| gptkbp:release_country |
capable of international missions
|
| gptkbp:reliability |
high reliability expected
|
| gptkbp:safety_features |
redundant systems
|
| gptkbp:stakeholders |
various stakeholders involved
|
| gptkbp:successor |
gptkb:Atlas_V
|
| gptkbp:support_for_science_missions |
supports scientific payloads
|
| gptkbp:sustainability_efforts |
aligned with sustainability goals.
|
| gptkbp:target_market |
government and commercial customers
|
| gptkbp:upgrades |
planned upgrades for performance
|
| gptkbp:bfsParent |
gptkb:United_Launch_Alliance_Vulcan_Centaur
|
| gptkbp:bfsLayer |
6
|