LK-700 Block 1V
Spacecraft · Russia
Original archive entry. The text, images and links below are kept as they were written.
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.
Spacecraft delta v: 2,804 m/s (9,199 ft/sec).
Related
- Family
- Manned spacecraft module
- Country
- Russia
- Spacecraft
- LK-700
- Propellants
- N2O4/UDMH