Jericho II-1

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Model: Jericho II-1. Gross Mass: 300 kg (660 lb). Thrust (vac): 20.000 kN (4,496 lbf). Burn time: 24 sec. Propellants: Solid. Diameter: 0.31 m (1.01 ft). Length: 2.70 m (8.80 ft). Country: Israel. No Engines: 1. Motor: Jericho II. Status: Active. First Flight: 1987. Last Flight: 2001. No Launched: 5. Used as: Belier. Release conditions: Sud. Used on Launch Vehicles: Jericho. 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.