RD-0110MD
RD-0110M
Credit - KBKhA
Manufacturer Name: RD-0110MD. Designer: Kosberg. Developed in: 1994-. Propellants: Lox/LNG. Thrust(vac): 245.000 kN (55,078 lbf). Burn time: 20 sec. Chambers: 4. Chamber Pressure: 54.00 bar. Area Ratio: 82.20. Country: Russia. Status: Developed 1994-on.

Prototype engine for tests with propellants LOX/liquified natural gas. Tests performed from 30 April 1998 on, test duration 20s.

Bibliography and Further Reading
  • Novosti kosmonavtiki, Issue 3, 1999.
 
 
 
 
 
 
 
 
 
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