RD-0132M

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RD-0132M

Part of RD-0131

Kosberg LOx/LNG rocket engine. Vozdushnyy Start stage 2. Design concept 1998-. Proposed variant of RD-0132, replacing hydrogen by liquid natural gas. Initially selected for stage 2 of Vozdushnyy Start project by Kompomash.

Status: Design concept 1998-. Date: 1998-. Thrust: 98.00 kN (22,031 lbf).

Chambers: 4.

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

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