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LK-700 Block 1V
Russian manned spacecraft module. Study 1968. Main engine of 13,400 kgf and three engines for soft landing / midcourse maneuvers of 1,670 kgf each. Trans-earth injection / midcourse man oeuvre stage.

AKA: Block 1V. Status: Study 1968. Thrust: 180.54 kN (40,587 lbf). Gross mass: 11,670 kg (25,720 lb). Unfuelled mass: 2,675 kg (5,897 lb).

Spacecraft delta v: 2,804 m/s (9,199 ft/sec).



Family: Manned spacecraft module. Country: Russia. Spacecraft: LK-700. Propellants: N2O4/UDMH.

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