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Model: Burya. Gross Mass: 40,865 kg (90,091 lb). Empty Mass: 13,000 kg (28,000 lb). Thrust (vac): 76.000 kN (17,085 lbf). Isp: 1,500 sec. Burn time: 8,500 sec. Propellants: Air/Kerosene. Isp(sl): 0 sec. Diameter: 2.20 m (7.20 ft). Span: 7.75 m (25.41 ft). Length: 18.00 m (59.00 ft). Country: Russia. No Engines: 1. Motor: RD-012U. Status: Retired 1960. First Flight: 1957. Last Flight: 1960. No Launched: 18. Other designations: La-X, Objekt 350. Payload: 2,350 kg (5,180 lb). Release velocity: 945 m/s (3,100 ft/sec). Release altitude: 19 m (62 ft). Release conditions: 3,200 kph at 19 km. Boosted by 2 x R-11 derivative boosters. 6,500 km tested, 8,000 km specified, cruise at Mach 3.2 at 18-20 km altitude with 2,350 kg warhead. Flight tested 1957 - 1960. Wing area 60 square meters; diameter of ramjet inlet 1.7 m. Total missile mass 97,215 kg; gross masses prorated, empty masses estimated. Used on Launch Vehicles: Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. |