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8S816
Part of UR-100-1 stage series Family

8K84 back

8K84 back
Credit: © Mark Wade

N2O4/UDMH propellant rocket stage. Orevo has sectioned hardware. Total mass, sea level thrust accurate; Isp, empty mass and burn time estimated. Source: Placard, Orevo.

AKA: 8K84 Stage 1. Status: Retired 1984. Thrust: 868.80 kN (195,314 lbf). Gross mass: 32,799 kg (72,309 lb). Unfuelled mass: 3,000 kg (6,600 lb). Specific impulse: 310 s. Specific impulse sea level: 280 s. Burn time: 102 s. Height: 10.00 m (32.00 ft). Diameter: 1.60 m (5.20 ft). Span: 1.60 m (5.20 ft).

No Engines: 4.



Country: Russia. Engines: RD-0215, RD-0217, RD-0216. Launch Vehicles: UR-100M SLBM, UR-100, UR-100K, UR-100M, UR-100U. Propellants: N2O4/UDMH.

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