|
gptkbp:instanceOf
|
rocket
|
|
gptkbp:associatedWith
|
gptkb:Space_Shuttle_program
gptkb:International_Space_Station
satellite launches
Lunar missions
Mars_exploration_missions
|
|
gptkbp:crewCapacity
|
3
|
|
gptkbp:designedBy
|
gptkb:Soviet_Union
|
|
gptkbp:diameter
|
10.3 meters
|
|
gptkbp:firstAwarded
|
2023
scheduled for 2024
RD-107
|
|
gptkbp:firstFlight
|
1966
|
|
gptkbp:firstMatch
|
RD-108
|
|
gptkbp:hasVersion
|
gptkb:Soyuz_2.1b
|
|
gptkbp:height
|
49.5 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz rocket
|
|
gptkbp:launched
|
approximately $50 million
approximately 5-10 per year
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
313,000 kg
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz
|
|
gptkbp:manufacturer
|
gptkb:Progress_Rocket_Space_Centre
|
|
gptkbp:notableFeature
|
gptkb:Soyuz_MS-10
gptkb:Soyuz_1
gptkb:Soyuz_11
gptkb:Soyuz_7
gptkb:Soyuz_T-10-1
gptkb:Soyuz_18a
modular design
international collaboration
high reliability
launch escape system
solid rocket boosters
long operational history
versatile payload options
automated docking system
adaptability for different missions
crew capsule
|
|
gptkbp:numberOfStudents
|
3
|
|
gptkbp:operatedBy
|
gptkb:Roscosmos
|
|
gptkbp:operationalStatus
|
1967
|
|
gptkbp:payloadCapacity
|
7,800 kg
|
|
gptkbp:percentageOfFamiliesBelowPovertyLine
|
RD-0110
|
|
gptkbp:reliability
|
no
high
|
|
gptkbp:retired
|
no
|
|
gptkbp:services
|
1967
|
|
gptkbp:succeededBy
|
over 90%
over 180 missions
|
|
gptkbp:usedBy
|
gptkb:European_Space_Agency
gptkb:Indian_Space_Research_Organisation
gptkb:Russian_space_agency
NASA
|
|
gptkbp:usedFor
|
human spaceflight
|