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Model: 8S816. 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. Motor: RD-0216. Status: Retired 1984. First Flight: 1969. Last Flight: 1984. No Launched: 115. 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. Model: UR-100N Stage 1N. Gross Mass: 77,150 kg (170,080 lb). Empty Mass: 5,695 kg (12,555 lb). Thrust (vac): 1,778.661 kN (399,859 lbf). Isp: 310 sec. Burn time: 121 sec. Propellants: N2O4/UDMH. Isp(sl): 285 sec. Diameter: 2.50 m (8.20 ft). Span: 2.50 m (8.20 ft). Length: 17.20 m (56.40 ft). Country: Russia. No Engines: 4. Motor: RD-0232. Status: Active. First Flight: 1972. Last Flight: 2007. No Launched: 178. No Failed: 1.
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