RD-0410
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
RD-0410 Nuclear Thermal Engine
Credit: © Dietrich Haeseler
Kosberg nuclear/LH2 rocket engine. Experimental nuclear engine, propellant LH2. Developed 1965-94. Tested at Semipalatinsk test range in 1980s and was "the only operational nuclear engine in the USSR". First flight 1985.
Engine: 2,000 kg (4,400 lb). Thrust to Weight Ratio: 1.8.
Related
- Family
- nuclear-powered
- Country
- Russia
- Propellants
- Nuclear/LH2
- Agency
- Kosberg bureau