RLA-1
RD-170

Credit - © Mark Wade
Gross Mass: 800,000 kg (1,760,000 lb). Empty Mass: 45,000 kg (99,000 lb). Thrust (vac): 11,700.000 kN (2,630,200 lbf). Isp: 337 sec. Burn time: 210 sec. Propellants: Lox/Kerosene. Isp(sl): 311 sec. Diameter: 6.00 m (19.60 ft). Span: 6.00 m (19.60 ft). Length: 30.00 m (98.00 ft). Country: USSR. No Engines: 1. Engine: RLA-1200. Status: Design 1974.

Empty mass, specific impulses, length estimated by comparison to smaller Zenit successor design.

Used on Launch Vehicles:  
 
 
 
 
 
 
 
 
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