Soyuz-2

GPTKB entity

Statements (63)
Predicate Object
gptkbp:instance_of gptkb:aircraft
gptkb:rocket
gptkbp:collaborations ESA and NASA
gptkbp:crew gptkb:3
gptkbp:debut_year over 30 launches
gptkbp:design replace older Soyuz models
gptkbp:developer 1990s to 2000s
gptkbp:diameter 10.3 meters
10.3 m
gptkbp:engine liquid-fueled
gptkbp:engine_type gptkb:RD-0124
gptkbp:family gptkb:Soyuz
gptkbp:first_flight gptkb:2004
2004-10-20
gptkbp:fuel_type RP-1 and liquid oxygen
gptkbp:guidance_system inertial navigation
gptkbp:height 46.3 meters
46.3 m
https://www.w3.org/2000/01/rdf-schema#label Soyuz-2
gptkbp:is_used_for crew and cargo transport
gptkbp:launch_date 2004-10-20
ongoing
frequent
gptkbp:launch_site gptkb:Baikonur_Cosmodrome
gptkbp:launch_vehicle gptkb:Soyuz
gptkb:aircraft
gptkb:Soyuz_family
operational
modular
medium-lift
commercial and governmental missions
Site 31/6
gptkbp:launched over 50
gptkbp:manufacturer gptkb:Russian_Federal_Space_Agency
gptkb:Progress_Rocket_Space_Centre
gptkbp:mission International Space Station resupply
gptkbp:notable_features enhanced reliability
increased payload capacity
improved avionics
gptkbp:number_of_stages gptkb:3
gptkbp:operated_by gptkb:Arianespace
gptkbp:operational_status gptkb:2004
active
gptkbp:primary_source satellite deployment
gptkbp:propulsion 400 k N
gptkbp:reliability high
98%+
gptkbp:seating_capacity gptkb:European_Space_Agency_satellites
gptkb:NASA_satellites
horizontal
7,800 kg
4.1 meters
up to 2,500 kg
Russian satellites
8000 kg to LEO
gptkbp:services gptkb:2004
gptkbp:setting gptkb:Soyuz-2.1b
gptkb:Soyuz-2.1v
gptkb:Soyuz-2.1a
gptkbp:succeeded_by 98%
gptkbp:successor gptkb:Soyuz-2.1b
gptkbp:bfsParent gptkb:spacecraft
gptkbp:bfsLayer 3