|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:boosterEngines
|
gptkb:RD-108
|
|
gptkbp:coreStageEngines
|
gptkb:RD-107
|
|
gptkbp:countryOfOrigin
|
gptkb:Soviet_Union
|
|
gptkbp:designer
|
gptkb:Sergei_Korolev
|
|
gptkbp:diameter
|
2.95 m
|
|
gptkbp:engineType
|
liquid-fueled
|
|
gptkbp:firstFlight
|
1957-05-15
|
|
gptkbp:firstICBM
|
true
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-7 family rockets
|
|
gptkbp:launchSite
|
gptkb:Plesetsk_Cosmodrome
gptkb:Vostochny_Cosmodrome
gptkb:Baikonur_Cosmodrome
Site 1/5
Site 31/6
Site 43/3
Site 43/4
|
|
gptkbp:length
|
34 m – 52 m
|
|
gptkbp:manufacturer
|
gptkb:Energia
|
|
gptkbp:nickname
|
Semyorka
|
|
gptkbp:notableFor
|
first artificial satellite launch
first human spaceflight
|
|
gptkbp:notableMission
|
gptkb:Luna_2
gptkb:Sputnik_1
gptkb:Vostok_1
Soyuz missions
|
|
gptkbp:notableVariant
|
gptkb:Soyuz
gptkb:Molniya
gptkb:Voskhod
gptkb:Luna
gptkb:Vostok
gptkb:Sputnik
|
|
gptkbp:numberOfLaunches
|
over 1800
|
|
gptkbp:numberOfStages
|
2
core plus four strap-on boosters
|
|
gptkbp:payloadToLEO
|
up to 7,800 kg
|
|
gptkbp:propulsion
|
kerosene
liquid oxygen
|
|
gptkbp:relatedTo
|
gptkb:Soyuz_rocket
gptkb:Sputnik_rocket
gptkb:Molniya_rocket
gptkb:Voskhod_rocket
gptkb:Vostok_rocket
gptkb:Luna_rocket
|
|
gptkbp:status
|
active
|
|
gptkbp:successRate
|
over 95%
|
|
gptkbp:usedBy
|
gptkb:Soviet_space_program
gptkb:Russian_space_program
|
|
gptkbp:usedFor
|
gptkb:satellite
gptkb:ICBM
|
|
gptkbp:bfsParent
|
gptkb:Korolev_cross_separation_pattern
|
|
gptkbp:bfsLayer
|
6
|