|
gptkbp:instanceOf
|
launch vehicle
|
|
gptkbp:controls
|
inertial guidance
|
|
gptkbp:crew
|
Cosmonaut training program
|
|
gptkbp:crewCapacity
|
3
yes
|
|
gptkbp:currentUse
|
ISS crew transport
|
|
gptkbp:decommissioned
|
no
|
|
gptkbp:designedBy
|
gptkb:Soviet_Union
|
|
gptkbp:engineType
|
RD-107 and RD-108
|
|
gptkbp:firstFlight
|
1966
2000
2023
|
|
gptkbp:fuelType
|
RP-1_and_Liquid_Oxygen
|
|
gptkbp:futurePlans
|
continued use for ISS missions
|
|
gptkbp:hasPartnershipsWith
|
NASA, ESA
|
|
gptkbp:height
|
49.5 meters
|
|
gptkbp:historicalSignificance
|
first spacecraft to carry humans to the ISS
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz Launch System
|
|
gptkbp:launched
|
varies
approximately $50 million
ground-based
multiple per year
approximately 10-15 per year
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
313,000 kg
over 180
mobile launch platform
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz_family
less than 10
|
|
gptkbp:manufacturer
|
gptkb:Progress_Rocket_Space_Centre
|
|
gptkbp:missions
|
gptkb:Moscow
|
|
gptkbp:modifications
|
multiple upgrades over the years
|
|
gptkbp:nextStation
|
2024
|
|
gptkbp:notableFeature
|
gptkb:Apollo-Soyuz_Test_Project
International_Space_Station_resupply
Soyuz_1,_Soyuz_7,_Soyuz_MS-10
|
|
gptkbp:number_of_stages
|
3
|
|
gptkbp:operationalArea
|
human spaceflight
|
|
gptkbp:operationalStatus
|
1967
active
|
|
gptkbp:orbitalInclination
|
yes
|
|
gptkbp:passenger_traffic
|
2.5 meters
|
|
gptkbp:payloadCapacity
|
7,800 kg
|
|
gptkbp:propulsion
|
1,000 kN
|
|
gptkbp:reliability
|
no
high
|
|
gptkbp:safetyFeatures
|
excellent
|
|
gptkbp:succeededBy
|
over 90%
|
|
gptkbp:supportRole
|
commercial satellite launches
|
|
gptkbp:usedBy
|
gptkb:Russian_space_agency
|