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1.12.1 Soyuz-T Specifications
- Launch weight .......................................... 6850 kg
- Length ..................................................... 6.98 m
- Span across solar arrays .......................... 10.6 m
- Diameter of habitable modules ................... 2.2 m
- Maximum diameter ................................... 2.72 m
- Habitable volume ...................................... 9.5 m3
- Number of crew ........................................ 2-3
1.12.2 Soyuz-T Notable Features
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- ↑ Pierre Langereux, “New Revelations on the Soyuz-T Vehicle,” Air & Cosmos , No. 800, February 16, 1980, pp. 50-51. Translated in JPRS Report, JPRS L/9058, USSR Report, Space, April 28, 1980, p. 2.
- ↑ Yuri Malyshev, “Evolution of the Soyuz Spacecraft,” Aviatsiya i Kosmonavtika, No. 10, 1980, pp. 38-39. Translated in USSR Report, Space, No. 9, March 2, 1981 (JPRS 77488), p. 11.