RD-2MZV

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RD-2MZV

Part of RD-1

Dushkin Nitric acid/Kerosene rocket engine. I-270. Developed 1944-47. Thrust variable 0.1-0.3 metric tons / 0.35-1.4 metric tons.

Status: Developed 1944-47. Date: 1944-47. Thrust: 13.70 kN (3,080 lbf).

Chambers: 2.

Family: Storable liquid. Country: Russia. Propellants: Nitric acid/Kerosene. Agency: Dushkin.

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