Glushko LOx/LNG rocket engine. Vozdushnyy Start stage 1. Developed 1998-. Variant of RD-182 engine for liquid natural gas (mainly CH4). Proposed initial candidate for project Vozdushnyy Start of Kompomash.
Status: Developed 1998-. Date: 1998-. Thrust: 882.00 kN (198,281 lbf).