This page no longer updated from 31 October 2001. Latest version can be found at LK-4

Gross Mass: 237 kg. Empty Mass: 71 kg. Thrust (vac): 41 kgf. Isp: 200 sec. Burn time: 800 sec. Propellants: Hydrazine Diameter: 1.6 m. Span: 1.6 m. Length: 1.3 m. Country: Israel. No Engines: 1. LK-4 Status: Hardware. Comments: Upper stage for orbital insertion of Shavit or Leolink payloads.
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Last update 12 March 2001.
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© Mark Wade, 2001 .