Soyuz T PAO

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Soyuz T PAO

Part of Soyuz

Russian manned spacecraft module. 18 launches, 1978.04.04 (Cosmos 1001) to 1986.03.13 (Soyuz T-15). Improved PAO service module derived from Soyuz 7K-S with pressure-fed main engines and unitary RCS/main engine propellant feed system. Equipment-engine section.

AKA: Priborno-agregatniy otsek. Status: Operational 1978. Thrust: 3.09 kN (694 lbf). Gross mass: 2,750 kg (6,060 lb). Unfuelled mass: 2,050 kg (4,510 lb). Specific impulse: 292 s. Height: 2.26 m (7.41 ft). Diameter: 2.15 m (7.05 ft).

RCS Coarse No x Thrust: 16 X 98 N. RCS Fine No x Thrust: 8 X 98 N. RCS Coarse Backup No x Thrust: No separate backup translation engines.. Electric System: 0.60 average kW.

Family: Manned spacecraft module. Country: Russia. Spacecraft: Soyuz T. Propellants: N2O4/UDMH.

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