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Soyuz TMA BO

Spacecraft · Russia

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

Russian manned spacecraft module. Operational. First launch 2002.10.30. Lightweight male/female docking system with flange-type probe, internal transfer tunnel. Kurs automatic rendezvous and docking system with two Kurs antennae, no tower. Living section.

Collar Length: 0.22 m. Probe Length: 0.50 m. Base Diameter: 1.35 m. Ring Diameter: 1.35 m. One window, BO separated after retrofire.

Habitable Volume: 5.00 m3.

Country
Russia
Spacecraft
Soyuz TMA