RD-0143 home
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Engine Model: RD-0143. Manufacturer Name: RD-0143. Designer: Kosberg. Developed in: 1998-. Application: Vozdushnyy Start stage 2. Propellants: Lox/LNG. Thrust(vac): 343.000 kN (77,109 lbf). Isp: 372 sec. Chambers: 4. Country: Russia. Status: Design concept 1998-.

Proposed variant of RD-0124, replacing kerosene by liquid natural gas. Selected for stage 2 of Vozdushnyy Start project by Kompomash.

Engine Model: RD-0143A. Manufacturer Name: RD-0143A. Designer: Kosberg. Developed in: 1998-. Application: Vozdushnyy Start stage 1. Propellants: Lox/LNG. Thrust(vac): 343.000 kN (77,109 lbf). Isp: 370 sec. Chambers: 1. Country: Russia. Status: Design concept 1998-.

Proposed single chamber variant of RD-0143. Selected for stage 1 of Vozdushnyy Start project by Kompomash.

Bibliography:

  • "Air-Launch aerospace complex", Leaflet by Kompomash and Polyot Aviation Company, ILA 97 via Dietrich Haeseler.
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