| LK-4 |
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Model: LK-4. Gross Mass: 237 kg (522 lb). Empty Mass: 71 kg (156 lb). Thrust (vac): 402 N (90 lbf). Isp: 200 sec. Burn time: 800 sec. Propellants: Hydrazine. Diameter: 1.56 m (5.11 ft). Span: 1.56 m (5.11 ft). Length: 1.30 m (4.20 ft). Country: Israel. No Engines: 1. Status: Development ended 2001. Upper stage for orbital insertion of Shavit or Leolink payloads. 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. |