LK-700 Block 11
Spacecraft · Russia
Original archive entry. The text, images and links below are kept as they were written.
Russian manned spacecraft module. Study 1968. Differed from the lateral Block 1 stages in having an engine unit for orientation of the assembly. Main engine of 23,500 kgf and three engines for soft landing / midcourse maneuvers of 1,670 kgf each. Midcourse man oeuvre/lunar braking stage.
Spacecraft delta v: 3,000 m/s (9,800 ft/sec).
Related
- Family
- Manned spacecraft module
- Country
- Russia
- Spacecraft
- LK-700
- Propellants
- N2O4/UDMH