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Burlak Stage 2
N2O4/UDMH propellant rocket stage. Masses, thrust, specific impulse estimated based on total vehicle mass of 28.5 metric tons and first stage burn time of 140 seconds. Air launched from Tu-160 at 13,500 m, Mach 1.7 release conditions.

Status: Development ended 1992. Thrust: 98.00 kN (22,031 lbf). Gross mass: 9,400 kg (20,700 lb). Unfuelled mass: 900 kg (1,980 lb). Specific impulse: 330 s. Specific impulse sea level: 230 s. Burn time: 275 s. Height: 5.50 m (18.00 ft). Diameter: 1.60 m (5.20 ft). Span: 1.60 m (5.20 ft).



Family: Storable liquid. Country: Russia. Launch Vehicles: Burlak. Propellants: N2O4/UDMH. Stages: Burlak Stage 2.

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