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RD-0110MD
Part of RD-0106 Family
RD-0110M
RD-0110M
Credit: KBKhA
Kosberg LOx/LNG rocket engine. Developed 1994-on. Prototype engine for tests with propellants LOX/liquefied natural gas. Tests performed from 30 April 1998 on, test duration 20s.

Status: Developed 1994-on. Date: 1994-. Thrust: 245.00 kN (55,078 lbf). Burn time: 20 s.

Chambers: 4. Chamber Pressure: 54.00 bar. Area Ratio: 82.2.



Country: Russia. Propellants: Lox/LNG. Agency: Kosberg bureau.

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