|
gptkbp:instanceOf
|
launch vehicle
|
|
gptkbp:crewCapacity
|
3
|
|
gptkbp:designedBy
|
gptkb:S.P._Korolev
|
|
gptkbp:diameter
|
10.3 meters
|
|
gptkbp:engineType
|
RD-107 and RD-108
|
|
gptkbp:firstAwarded
|
core stage
|
|
gptkbp:firstClaim
|
upper stage
|
|
gptkbp:firstFlight
|
ongoing
1966-11-28
1967-04-23
|
|
gptkbp:firstMatch
|
strap-on boosters
|
|
gptkbp:gameFeatures
|
RP-1_and_Liquid_Oxygen
|
|
gptkbp:hasPartnershipsWith
|
gptkb:JAXA
gptkb:ESA
NASA
|
|
gptkbp:height
|
49.5 meters
|
|
gptkbp:historicalSignificance
|
longest-serving launch vehicle
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz launch vehicle
|
|
gptkbp:launched
|
varies
frequent
ground control
approximately $50 million
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
vertical launch
|
|
gptkbp:manufacturer
|
gptkb:Progress_Rocket_Space_Centre
|
|
gptkbp:notableFeature
|
gptkb:Soyuz_MS-19
gptkb:Soyuz_MS-10
gptkb:Soyuz_MS-23
gptkb:Soyuz_MS-15
gptkb:Soyuz_MS-16
gptkb:Soyuz_1
gptkb:Mars_3
gptkb:Soyuz_MS-11
gptkb:Soyuz_MS-17
gptkb:Soyuz_MS-24
gptkb:Hubble_Space_Telescope
gptkb:Soyuz_MS-13
gptkb:Soyuz_MS-18
gptkb:Soyuz_MS-21
gptkb:Soyuz_11
gptkb:Soyuz_MS-20
gptkb:Soyuz_MS-12
gptkb:Soyuz_TMA-1
gptkb:Soyuz_MS-22
gptkb:Soyuz_MS-14
Luna 9
Venera 7
International_Space_Station_resupply
|
|
gptkbp:number_of_stages
|
3
|
|
gptkbp:operatedBy
|
gptkb:Roscosmos
|
|
gptkbp:operationalStatus
|
1967
|
|
gptkbp:payloadCapacity
|
7,800 kg
|
|
gptkbp:releaseFormat
|
gptkb:Gagarin's_Start
|
|
gptkbp:reliability
|
high
not_reusable
|
|
gptkbp:safetyFeatures
|
good
|
|
gptkbp:succeededBy
|
over 90%
|
|
gptkbp:usedBy
|
gptkb:Russian_space_agency
|
|
gptkbp:usedFor
|
satellite launches
crewed spaceflights
cargo missions
|
|
gptkbp:weight
|
313,000 kg
|