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RD-0143
Part of RD-0106 Family
Kosberg LOx/LNG rocket engine. Vozdushnyy Start stage 2. Design concept 1998-. Proposed variant of RD-0124, replacing kerosene by liquid natural gas. Selected for stage 2 of Vozdushnyy Start project by Kompomash.

Status: Design concept 1998-. Date: 1998-. Thrust: 343.00 kN (77,109 lbf). Specific impulse: 372 s.

Chambers: 4.



Country: Russia. Propellants: Lox/LNG. Agency: Kosberg bureau. Bibliography: 328.

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