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RD-0132M
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Manufacturer Name: RD-0132M. Designer: Kosberg. Developed in: 1998-. Application: Vozdushnyy Start stage 2. Propellants: Lox/LNG. Thrust(vac): 98.000 kN (22,031 lbf). Chambers: 4. Country: Russia. Status: 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.
Bibliography and Further Reading - Polovnikov S P; Karpov, A S, Vestnik Aviatsii i Kosmonavtiki, "Projekt 'Vozdushnyy Start'", Moscow, 1-2/98 via Dietrich Haeseler.
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