|
gptkbp:instance_of
|
gptkb:Space_Launch_System
|
|
gptkbp:check_in_time
|
150 seconds
|
|
gptkbp:configuration
|
medium-lift
|
|
gptkbp:country_of_origin
|
gptkb:Russia
|
|
gptkbp:crew_capacity
|
gptkb:none
|
|
gptkbp:debut
|
multiple successful launches
2011-10-20
|
|
gptkbp:design_purpose
|
commercial satellite launch
|
|
gptkbp:diameter
|
10.3 meters
|
|
gptkbp:engine_type
|
gptkb:RD-0124
|
|
gptkbp:first_flight
|
2023-09-30
2011-10-20
|
|
gptkbp:fuel_type
|
RP-1 and liquid oxygen
|
|
gptkbp:guidance_system
|
inertial guidance system
|
|
gptkbp:has_tour
|
staged combustion
|
|
gptkbp:height
|
46.3 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz ST
|
|
gptkbp:launch_date
|
frequent
|
|
gptkbp:launch_event
|
over 90%
|
|
gptkbp:launch_platform
|
gptkb:Arianespace
ground launch
|
|
gptkbp:launch_price
|
approximately $50 million
|
|
gptkbp:launch_site
|
gptkb:Centre_Spatial_Guyanais
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz
gptkb:Team_Rocket
|
|
gptkbp:launch_window
|
varies
|
|
gptkbp:manufacturer
|
gptkb:Russian_Federal_Space_Agency
|
|
gptkbp:mass
|
313,000 kg
|
|
gptkbp:mission
|
direct injection
|
|
gptkbp:notable_launches
|
gptkb:Galileo_satellites
|
|
gptkbp:number_of_engines
|
gptkb:4
|
|
gptkbp:number_of_stages
|
gptkb:3
|
|
gptkbp:operational_since
|
gptkb:2011
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:payload_capacity
|
3,000 kg
3.4 meters
7,800 kg
multiple payloads
10.0 meters
|
|
gptkbp:propulsion
|
1,000 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:successor
|
gptkb:Soyuz_2
|
|
gptkbp:used_for
|
satellite launches
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:bfsLayer
|
4
|