This page no longer updated from 31 October 2001. Latest version can be found at RD-0143A

Manufacturer Name: RD-0143A. Designer: Kosberg. Developed in: 1998-. Application: Vozdushnyy Start stage 1. Propellants: Lox/LNG Thrust(vac): 35,000 kgf. Thrust(vac): 343.00 kN. Isp: 370 sec. Chambers: 1. Country: Russia. Status: Design concept 1998-. References: 328 . Comments: Proposed single chamber variant of RD-0143. Selected for stage 1 of Vozdushnyy Start project by Kompomash.
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Last update 12 March 2001.
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© Mark Wade, 2001 .