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4D10
Isayev N2O4/UDMH rocket engine. R-27 / RSM-25 (SS-N-6). Out of Production. First engine system to be submerged in propellant tank. One main engine chamber plus unknown number (probably 4) of steering thrusters. Thrust 226 + 29 kN.

Status: Out of Production. Thrust: 255.00 kN (57,326 lbf).

Chambers: 1 + 4.

Family: Storable liquid. Country: Russia. Launch Vehicles: R-27. Propellants: N2O4/UDMH. Agency: Isayev bureau. Bibliography: 319, 340, 342.
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