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Dnepr (rocket)
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== Performance == The Dnepr launch vehicle had only a small number of modifications compared to the R-36M ICBM in service. The main difference was the payload adapter located in the space head module and modified flight-control unit. This baseline version could lift 3,600 kg into a 300 km [[low Earth orbit]] at an [[inclination]] of 50.6Β°, or 2,300 kg to a 300 km [[Sun-synchronous orbit]] at an inclination of 98.0Β°. On a typical mission the Dnepr deployed a larger main payload and a secondary payload of [[Miniaturized satellite]]s and [[CubeSat]]s.
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