Soyuz 7K-L1 SA

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Soyuz 7K-L1 SA

Part of Soyuz

Russian manned spacecraft module. 12 launches, 1967.03.10 (Cosmos 146) to 1970.10.20 (Zond 8). Increased heat shield protection and presumably reaction control system propellant for re-entry from lunar distances. Reentry capsule.

AKA: Spuskaemiy apparat. Status: Operational 1967. Gross mass: 2,800 kg (6,100 lb). Unfuelled mass: 2,700 kg (5,900 lb). Height: 2.24 m (7.34 ft). Diameter: 2.17 m (7.11 ft).

Reserve parachute deleted and hatch for entry of crew through side of spacecraft added. Crew of two provided with Orlan space suits and parachutes for bail-out through side hatch in event of failure of main parachute.

Crew Size: 2. Habitable Volume: 4.00 m3. RCS Coarse No x Thrust: 6 X 98 N.

Family: Manned spacecraft module. Country: Russia. Spacecraft: Soyuz 7K-L1.

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