United Launch Alliance's Vulcan Centaur rocket
GPTKB entity
Statements (56)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Team_Rocket
|
| gptkbp:academic_programs |
experienced engineering team involved
|
| gptkbp:configuration |
multiple configurations available
|
| gptkbp:contract |
awarded contracts for national security missions
|
| gptkbp:contracted_launches |
NASA and U. S. Department of Defense
|
| gptkbp:control_system |
advanced avionics
|
| gptkbp:crew_capacity |
uncrewed missions planned
|
| gptkbp:customer_support |
dedicated customer support team
|
| gptkbp:development_cost |
estimated at $1 billion
|
| gptkbp:diameter |
5.4 meters
|
| gptkbp:durability |
partially reusable
|
| gptkbp:engine |
BE-4 developed by Blue Origin
|
| gptkbp:engine_type |
BE-4 and Centaur V
|
| gptkbp:environmental_impact |
designed to minimize environmental impact
|
| gptkbp:first_flight |
gptkb:2023
|
| gptkbp:future_plans |
upgrades planned for future missions
|
| gptkbp:height |
approximately 60 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
United Launch Alliance's Vulcan Centaur rocket
|
| gptkbp:innovation |
incorporates new technologies
|
| gptkbp:intended_use |
satellite launches
|
| gptkbp:is_tested_for |
extensive testing program
|
| gptkbp:launch_date |
up to 12 launches per year
|
| gptkbp:launch_platform |
detailed post-launch analysis conducted
state-of-the-art launch control systems |
| gptkbp:launch_price |
competitive launch pricing
|
| gptkbp:launch_site |
gptkb:Cape_Canaveral_Space_Force_Station
|
| gptkbp:launch_vehicle |
part of a new generation of launch vehicles
|
| gptkbp:launch_window |
flexible launch windows available
|
| gptkbp:launched |
thorough launch preparation procedures
|
| gptkbp:manufacturer |
gptkb:United_Launch_Alliance
|
| gptkbp:marketed_as |
available for commercial satellite launches
|
| gptkbp:media_coverage |
extensive media coverage expected
|
| gptkbp:mission |
high success rate expected
low Earth orbit and geostationary orbit |
| gptkbp:mission_diversity |
capable of diverse mission profiles
|
| gptkbp:number_of_stages |
two
|
| gptkbp:orbital_altitude |
capable of orbital maneuvering
|
| gptkbp:partnerships |
collaborations with various aerospace companies
|
| gptkbp:payload_capacity |
5.4-meter diameter
up to 27,200 kg to LEO efficient payload integration process various payload adapters available |
| gptkbp:project |
on schedule for first launch
incorporating future technologies in design |
| gptkbp:public_interest |
high public interest in launches
|
| gptkbp:release_country |
available for international customers
|
| gptkbp:replaces |
gptkb:Atlas_V
|
| gptkbp:safety_features |
redundant systems
|
| gptkbp:supply_chain |
robust supply chain established
|
| gptkbp:supports |
modernized ground systems
|
| gptkbp:sustainability_efforts |
aligned with sustainability goals
|
| gptkbp:training_programs |
training programs for customers
|
| gptkbp:uses |
liquid propellant
|
| gptkbp:bfsParent |
gptkb:BE-4_engine
gptkb:Blue_Origin's_BE-4 |
| gptkbp:bfsLayer |
5
|