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gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:air_traffic_control
|
autonomous flight control system
|
|
gptkbp:associated_with
|
gptkb:US_Air_Force
gptkb:NASA
commercial payloads
|
|
gptkbp:configuration
|
Common Booster Core
|
|
gptkbp:control_system
|
thrust vector control
|
|
gptkbp:debut
|
multiple successful missions
over 30 launches conducted
|
|
gptkbp:design
|
modular design
|
|
gptkbp:design_purpose
|
to deliver payloads to various orbits
|
|
gptkbp:diameter
|
5.1 meters
|
|
gptkbp:durability
|
not reusable
|
|
gptkbp:engine_type
|
gptkb:RL10
|
|
gptkbp:environmental_impact
|
minimized emissions
|
|
gptkbp:first_flight
|
gptkb:2002
gptkb:2023
|
|
gptkbp:future_plans
|
upgrades planned
|
|
gptkbp:guidance_system
|
gptkb:navigation_system
|
|
gptkbp:has_programs
|
gptkb:Evolved_Expendable_Launch_Vehicle_(EELV)
|
|
gptkbp:height
|
4.6 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Delta IV upper stage
|
|
gptkbp:integration
|
short integration time
|
|
gptkbp:launch_date
|
varies annually
|
|
gptkbp:launch_platform
|
gptkb:United_Launch_Alliance
|
|
gptkbp:launch_price
|
varies by mission
|
|
gptkbp:launch_site
|
gptkb:Vandenberg_Space_Force_Base
gptkb:Cape_Canaveral_Space_Force_Station
|
|
gptkbp:launch_vehicle
|
Delta family
|
|
gptkbp:launch_window
|
varies by mission
|
|
gptkbp:launched
|
ground support equipment required
|
|
gptkbp:manufacturer
|
gptkb:United_Launch_Alliance
|
|
gptkbp:mass
|
2,500 kg
|
|
gptkbp:mission
|
geostationary transfer orbit missions
high mission success rate
|
|
gptkbp:mission_type
|
scientific, commercial, and military missions
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:operational_since
|
gptkb:2002
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:operational_use
|
military and civilian missions
|
|
gptkbp:orbital_altitude
|
precise orbital insertion capabilities
|
|
gptkbp:payload_capacity
|
5-meter diameter
up to 5,000 kg to geostationary transfer orbit
flexible payload integration options
|
|
gptkbp:performance
|
high performance
|
|
gptkbp:propulsion
|
liquid hydrogen and liquid oxygen
25,000 lbf
|
|
gptkbp:reliability
|
proven
|
|
gptkbp:role
|
payload delivery to orbit
|
|
gptkbp:safety_record
|
excellent
|
|
gptkbp:success_rate
|
high
|
|
gptkbp:support
|
satellite deployment
|
|
gptkbp:technology
|
advanced propulsion technology
|
|
gptkbp:used_in
|
gptkb:Delta_IV_rocket
|
|
gptkbp:user_countries
|
used by international customers
|
|
gptkbp:bfsParent
|
gptkb:RL10_engine
|
|
gptkbp:bfsLayer
|
5
|