|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:countryOfOrigin
|
gptkb:Soviet_Union
gptkb:Ukraine
|
|
gptkbp:diameter
|
3.9 m
|
|
gptkbp:engineFirstStage
|
gptkb:RD-171
|
|
gptkbp:engineSecondStage
|
gptkb:RD-120
|
|
gptkbp:family
|
gptkb:Zenit-3SL
gptkb:Zenit-2M
gptkb:Zenit-2
gptkb:Zenit-3SLB
|
|
gptkbp:firstFlight
|
13 April 1985
|
|
gptkbp:firstStageReusable
|
no
|
|
gptkbp:height
|
57 m (Zenit-3SL)
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Zenit rocket family
|
|
gptkbp:launchSite
|
gptkb:Plesetsk_Cosmodrome
gptkb:Baikonur_Cosmodrome
gptkb:Sea_Launch_platform
|
|
gptkbp:manufacturer
|
gptkb:Yuzhnoye_Design_Bureau
gptkb:Yuzhmash
|
|
gptkbp:mass
|
471,000 kg (Zenit-3SL)
|
|
gptkbp:notableFeature
|
designed as a replacement for R-7 family
first Soviet rocket designed for automated launch
high performance for its class
used for Energia booster strap-ons
used for Sea Launch commercial launches
|
|
gptkbp:notableMission
|
gptkb:AngoSat-1
gptkb:Elektro-L_No.1
Sea Launch missions
Tselina-D satellites
|
|
gptkbp:numberOfLaunches
|
over 80
|
|
gptkbp:numberOfStages
|
2
|
|
gptkbp:payloadToGTO
|
3,600 kg (Zenit-3SL)
|
|
gptkbp:payloadToLEO
|
13,740 kg (Zenit-2)
|
|
gptkbp:predecessor
|
gptkb:R-7_rocket_family
|
|
gptkbp:propulsion
|
gptkb:RP-1
liquid oxygen
|
|
gptkbp:relatedTo
|
gptkb:Energia_rocket
gptkb:Sea_Launch
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
none
|
|
gptkbp:usedBy
|
gptkb:Land_Launch
gptkb:Sea_Launch
gptkb:Russia
gptkb:Soviet_Union
gptkb:Ukraine
|
|
gptkbp:usedFor
|
interplanetary missions
orbital launches
satellite launches
|
|
gptkbp:bfsParent
|
gptkb:Zenit-2SB
|
|
gptkbp:bfsLayer
|
6
|