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Soyuz T BO

Spacecraft · Russia

Original archive entry. The text, images and links below are kept as they were written.

Russian manned spacecraft module. 18 launches, 1978.04.04 (Cosmos 1001) to 1986.03.13 (Soyuz T-15). Lightweight male/female docking system with flange-type probe, internal transfer tunnel. Igla automatic rendezvous and docking system. Living section.

Collar Length: 0.22 m. Probe Length: 0.50 m. Base Diameter: 1.35 m. Ring Diameter: 1.35 m. Igla automatic rendezvous and docking system with lightweight antennae, lightweight tower. One window, BO separated before retrofire.

Habitable Volume: 5.00 m3.

Country
Russia
Spacecraft
Soyuz T