Soyuz 7K-OKS PAO
Spacecraft · Russia
Original archive entry. The text, images and links below are kept as they were written.
Russian manned spacecraft module. 2 launches, 1971.04.23 (Soyuz 10) to 1971.06.06 (Soyuz 11). Soyuz 7K-OK basic PAO service module with pump-fed main engines and separate RCS/main engine propellant feed system. Equipment-engine section.
Rear toroid housed Igla electronics, with outside diameter of 2.20 m and cross-section diameter 0.35 m.
RCS Coarse No x Thrust: 14 X 98 N. RCS Fine No x Thrust: 4 X 98 N. RCS Coarse Backup No x Thrust: 8 x 10 N. RCS Fine Backup No x Thrust: 4 x 10 N roll. Electric System: 0.50 average kW.
Related
- Family
- Manned spacecraft module
- Country
- Russia
- Spacecraft
- Soyuz 7KT-OK
- Propellants
- Nitric acid/Hydrazine