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Burlak Stage 1
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: 357.90 kN (80,459 lbf). Gross mass: 18,000 kg (39,000 lb). Unfuelled mass: 1,800 kg (3,900 lb). Specific impulse: 320 s. Specific impulse sea level: 270 s. Burn time: 140 s. Height: 10.50 m (34.40 ft). Diameter: 1.60 m (5.20 ft). Span: 1.90 m (6.20 ft).



Family: Storable liquid. Country: Russia. Launch Vehicles: Burlak. Propellants: N2O4/UDMH. Stages: Burlak Stage 1.

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