|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:countryOfOrigin
|
gptkb:Soviet_Union
|
|
gptkbp:designer
|
gptkb:Sergei_Korolev
|
|
gptkbp:diameter
|
2.95 m (core stage)
|
|
gptkbp:family
|
gptkb:Soyuz
gptkb:Molniya
gptkb:Voskhod
gptkb:R-7_Semyorka
gptkb:Luna
gptkb:Vostok
|
|
gptkbp:firstFlight
|
1957-05-15
|
|
gptkbp:fuelType
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-7 (rocket family)
|
|
gptkbp:launched
|
>1800
|
|
gptkbp:launchSite
|
gptkb:Plesetsk_Cosmodrome
gptkb:Vostochny_Cosmodrome
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:length
|
34 m (typical)
|
|
gptkbp:manufacturer
|
gptkb:OKB-1
|
|
gptkbp:mass
|
~280,000 kg (typical)
|
|
gptkbp:notableFor
|
first artificial satellite launch
first human spaceflight
first ICBM
basis for Soviet and Russian crewed spaceflight
world's most-launched rocket family
|
|
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
|
|
gptkbp:numberOfStages
|
2
|
|
gptkbp:oxidizer
|
liquid oxygen
|
|
gptkbp:predecessor
|
none
|
|
gptkbp:propulsion
|
gptkb:water
|
|
gptkbp:status
|
active
|
|
gptkbp:successor
|
none (still in use)
|
|
gptkbp:thrust
|
3.9 MN (typical at liftoff)
|
|
gptkbp:usedFor
|
gptkb:satellite
gptkb:ICBM
|
|
gptkbp:bfsParent
|
gptkb:Soyuz-2
|
|
gptkbp:bfsLayer
|
5
|