|
gptkbp:instance_of
|
gptkb:Space_Launch_System
|
|
gptkbp:collaboration
|
ESA and Arianespace
|
|
gptkbp:competitors
|
competes with Falcon 1 and Electron
|
|
gptkbp:configuration
|
two configurations
|
|
gptkbp:customer_support
|
gptkb:European_Space_Agency
|
|
gptkbp:debut
|
multiple successful launches
|
|
gptkbp:design
|
15 years
|
|
gptkbp:design_purpose
|
to enhance payload capacity
|
|
gptkbp:development
|
gptkb:European_Space_Agency
|
|
gptkbp:development_cost
|
approximately €300 million
|
|
gptkbp:engine_type
|
solid and liquid
|
|
gptkbp:environmental_concerns
|
designed for reduced emissions
|
|
gptkbp:first_flight
|
gptkb:2021
|
|
gptkbp:height
|
30 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Vega C Launch Vehicle
|
|
gptkbp:integration
|
shorter than previous models
|
|
gptkbp:launch_date
|
up to 12 per year
|
|
gptkbp:launch_price
|
approximately €35 million
|
|
gptkbp:launch_site
|
gptkb:Guiana_Space_Centre
|
|
gptkbp:launch_vehicle
|
over 95%
expendable launch vehicle
Vega family
light launch vehicle
|
|
gptkbp:manufacturer
|
gptkb:Arianespace
|
|
gptkbp:maximum_payload_to_sso
|
1,500 kg
|
|
gptkbp:mission
|
gptkb:LARES_2
polar and sun-synchronous orbits
planned for various payloads
|
|
gptkbp:number_of_stages
|
gptkb:3
P80
Zefiro 23
Avum+
|
|
gptkbp:operated_by
|
gptkb:Arianespace
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:payload_capacity
|
3 meters
2,500 kg
|
|
gptkbp:primary_use
|
small satellite launches
|
|
gptkbp:reliability
|
high
|
|
gptkbp:replaces
|
Vega C's predecessor
|
|
gptkbp:successor
|
gptkb:Vega_launch_vehicle
|
|
gptkbp:supports
|
modernized
|
|
gptkbp:target_market
|
small to medium satellites
|
|
gptkbp:technology
|
gptkb:advanced_propulsion_systems
|
|
gptkbp:bfsParent
|
gptkb:Astrium_Space_Transportation
|
|
gptkbp:bfsLayer
|
7
|