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8S816
Part of UR-100-1 stage series
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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