This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 40,865 kg.
Empty Mass: 13,000 kg. Thrust (vac): 7,750 kgf. Isp: 1,500 sec. Burn time: 8,500 sec. Propellants: Air/Kerosene Isp(sl): 0 sec. Diameter: 2.2 m. Span: 7.7 m. Length: 18.0 m. Country: Russia. No Engines: 1. RD-012U Status: Hardware. Other designations: La-X, Objekt 350.
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.
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Last update 12 March 2001.
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© Mark Wade, 2001 .