UR-200 Stage 2
RD-0205 8D46
RD-0205 8D46 on stage 8S816 (UR-200)
Credit - © Mark Wade
Gross Mass: 25,810 kg (56,900 lb). Empty Mass: 2,400 kg (5,200 lb). Thrust (vac): 612.900 kN (137,785 lbf). Isp: 322 sec. Burn time: 113 sec. Propellants: N2O4/UDMH. Diameter: 2.20 m (7.20 ft). Span: 2.20 m (7.20 ft). Length: 10.00 m (32.00 ft). Country: Russia. No Engines: 1. Engine: RD-0205. First Flight: 1963. Last Flight: 1964. No Launched: 9. Other designations: 8K81 Stage 2.

Tsniimash has 1:10 structural simulation model. Developed 1960-1965. Orevo has sectioned hardware. All data accurate except empty mass prorated between first and second stages.

Used on Launch Vehicles:  
 
 
 
 
 
 
 
 
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