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11D79
Stepanov N2O4/UDMH rocket engine. Blok D SOZ. In Production. Thrust 1.1-4.5 metric tons variable.

Status: In Production. Date: 1964-67. Thrust: 44.00 kN (9,891 lbf).



Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Stages: N1 Block D, Proton 11S824, Proton 11S824M, Proton 11S86, Proton 11S824F, Proton 17S40, Proton 11S861, Proton 11S861-01. Agency: Stepanov Design Bureau.

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