Progress M PAO

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Progress M PAO

Part of Soyuz

Russian manned spacecraft module. Operational, first launch 1989.08.23 (Progress M-1). 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 1989. Thrust: 6.20 kN (1,393 lbf). Gross mass: 2,950 kg (6,500 lb). Unfuelled mass: 2,070 kg (4,560 lb). Specific impulse: 302 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: Progress M, Progress M-SO. Propellants: N2O4/UDMH.

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