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Isayev 218
Isayev Nitric acid/Amine rocket engine.

Status: Out of Production. Thrust: 166.00 kN (37,318 lbf).

Thrust (sl): 166.000 kN (37,318 lbf). Thrust (sl): 17,000 kgf. Propellant Formulation: AK27I/TG-02.

Family: Storable liquid. Country: Russia. Launch Vehicles: S-25. Propellants: Nitric acid/Amine. Agency: Isayev bureau.
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