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KRR-300
Dushkin rocket engine. G-300. Developed 1955-62. Thrust variable 0.1 / 3.0 / 10 metric tons thrust.

Status: Developed 1955-62. Date: 1955-62. Thrust: 98.00 kN (22,031 lbf).

Chambers: 3.

Family: Storable liquid. Country: Russia. Agency: Dushkin.
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