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8S817
AKA: 8K84 Stage 2. Status: Retired 1984. Thrust: 131.45 kN (29,551 lbf). Gross mass: 8,611 kg (18,984 lb). Unfuelled mass: 900 kg (1,980 lb). Specific impulse: 325 s. Burn time: 184 s. Height: 6.69 m (21.95 ft). Diameter: 2.00 m (6.50 ft). Span: 1.30 m (4.20 ft).
Country: Russia. Engines: 8D423, Izotov UR-100 stage 2 vernier. Launch Vehicles: UR-100M SLBM, UR-100, UR-100K, UR-100M, UR-100U. Propellants: N2O4/UDMH.
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