S1.35800 (original) (raw)

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S1.35800

Part of S1

Korolev LOx/Kerosene rocket engine. R-7 verniers. Out of Production. Thrust variable 2.5-3.1 metric tons

Status: Out of Production. Date: 1954-57. Thrust: 30.00 kN (6,744 lbf).

Country: Russia. Launch Vehicles: R-7. Propellants: Lox/Kerosene. Agency: Korolev bureau.

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