UR-100 Stage 1
8K84 back

Credit - © Mark Wade
Gross Mass: 32,799 kg (72,309 lb). Empty Mass: 3,000 kg (6,600 lb). Thrust (vac): 868.800 kN (195,314 lbf). Isp: 310 sec. Burn time: 102 sec. Propellants: N2O4/UDMH. Isp(sl): 280 sec. Diameter: 1.60 m (5.20 ft). Span: 1.60 m (5.20 ft). Length: 10.00 m (32.00 ft). Country: Russia. No Engines: 4. Engine: RD-0216. Status: Design 1964. First Flight: 1965. Last Flight: 1984. No Launched: 282. Other designations: 8K84 Stage 1.

Orevo has sectioned hardware. Total mass, sea level thrust accurate; Isp, empty mass and burn time estimated. Source: Placard, Orevo.

Used on Launch Vehicles:  
 
 
 
 
 
 
 
 
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