Soyuz

Definition and stakes

Portrait of David S. F. Portree David S. F. Portree Mir Hardware Heritage — Part 1 - Soyuz

Since the launch of Salyut 6 in 1977, the Soviet/Russian station programs have had the following attributes with implications for Soyuz evolution:
Multiple docking ports Design lifetimes of more than 1 year, with the option to remain in orbit for several years through onorbit repairs, upgrades, and refurbishment Extended-duration stays by teams of two or three cosmonauts Extended-duration stays called for resupply, which in turn called for a specialized resupply spacecraft.
Source: Wikisource

Portrait of David S. F. Portree David S. F. Portree Mir Hardware Heritage — Part 1 - Soyuz

The Original Soyuz played much the same role in the Soviet manned lunar program as Gemini did in the U.S. manned lunar program. That is, it provided experience in essential techniques and technologies for lunar flight.
Figure 1-7. Soyuz rocket. With more than 1000 launches to its credit since 1963, the two-and-a-half-stage Soyuz rocket has flown more than any other. Propellants are liquid oxygen and kerosene. Weight of payload launched to 200-km, 51° circular orbit is 7000 kg. Figure 1-6. Original Soyuz spacecraft. Figure 1-8. Original Soyuz probe and drogue docking system.
Source: Wikisource

Portrait of David S. F. Portree David S. F. Portree Mir Hardware Heritage — Part 1 - Soyuz

When the Soyuz closed to within 25 km of the Salyut, the automatic rendezvous phase of operations commenced. The two vehicles sensed each other and the automatic rendezvous radio equipment (the Igla system) switched on. The spacecraft maneuvered to keep their Igla antennas in line-of-sight so the Soyuz unit could obtain data on range, speed of approach, and orientation. The control computer on the Soyuz Ferry operated the main and docking and orientation engines based on the input data.
Source: Wikisource

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