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15D13
Klimov N2O4/UDMH rocket engine. Study 1968. Main engine for midcourse Block 1V ascent/trans-earth injection stage of LK-700 manned spacecraft. See also 11D423.

Status: Study 1968. Thrust: 131.40 kN (29,540 lbf).

Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Agency: Klimov. Bibliography: 443.
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