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LK-1
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Gross Mass: 13,990 kg (30,840 lb). Empty Mass: 1,240 kg (2,730 lb). Thrust (vac): 774.000 kN (174,002 lbf). Isp: 268 sec. Burn time: 55 sec. Propellants: Solid. Isp(sl): 250 sec. Diameter: 1.35 m (4.42 ft). Span: 1.50 m (4.90 ft). Length: 7.50 m (24.60 ft). Country: Israel. No Engines: 1. Engine: LK-1. Status: In production. First Flight: 1995. Last Flight: 2004. No Launched: 4. Used as: Shavit-1; NEXT-1; RSA-3 - 1. Lengthened version of Shavit/RSA-3 rocket motor. For lower stage use with 17.1:1 nozzle. Fitted with 23.6:1 nozzle for upper stage use specific impulse increases to 279 seconds, length to 8.4 m, and empty and gross mass are increased by 135 kg.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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