Engine Model: RD-0145. Manufacturer Name: RD-0145. Designer: Kosberg. Developed in: 1998-. Application: upper stage. Propellants: Lox/LNG. Thrust(vac): 147.000 kN (33,046 lbf). Isp: 374 sec. Mass Engine: 282 kg (621 lb). Length: 1.42 m (4.65 ft). Chambers: 4. Thrust to Weight Ratio: 53.19. Country: Russia. Status: Developed 1998-on. Proposed engine for LOX/liquid natural gas. Staged combustion cycle. Four-chamber variant of RD-0144.
Bibliography:- Novosti kosmonavtiki, Issue 3, 1999.