UR-100N Stage 2N (original) (raw)
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UR-100N Stage 2N
N2O4/UDMH propellant rocket stage. Engine has one main engine and four verniers. Verniers continue to burn for 19 seconds after main stage shutoff.
Status: Active. Thrust: 214.27 kN (48,170 lbf). Gross mass: 12,195 kg (26,885 lb). Unfuelled mass: 1,485 kg (3,273 lb). Specific impulse: 322 s. Burn time: 183 s. Height: 3.90 m (12.70 ft). Diameter: 2.50 m (8.20 ft). Span: 2.50 m (8.20 ft).
Country: Russia. Engines: RD-0235, RD-0236. Launch Vehicles: UR-100N, UR-100NU 15A35, UR-100NU 15A35S, UR-100NU 15A35P, Rokot, Rokot K, Strela launch vehicle. Propellants: N2O4/UDMH.
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