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Short range ballistic missile. Year: 1990. Family: Jericho. Country: Israel. Follow-on version differed from original French-derived Jericho. Probably used single 4500 kg solid-propellant motor. Manufacturer: IAI. Location: Be'er Yaakov, Israel. Launches: 3. First Launch Date: 1990-12-21. Last Launch Date: 2000-04-06. Launch data is: incomplete. Apogee: 100 km (60 mi). Total Mass: 4,500 kg (9,900 lb). Core Diameter: 1.01 m (3.31 ft). Total Length: 10.06 m (33.00 ft). Span: 1.01 m (3.31 ft). Standard warhead mass: 500 kg (1,100 lb). Maximum range: 480 km (290 mi). Boost Propulsion: Solid rocket.
Jericho 1 Chronology 1990 December 21 - Launch Site: Negev. Launch Vehicle: Jericho 1. - Operational Test mission Nation: Israel. Agency: IDF. Apogee: 100 km (60 mi). References: 1823.
1991 October 30 - Launch Site: Negev. Launch Vehicle: Jericho 1. - Operational Test mission Nation: Israel. Agency: IDF. Apogee: 100 km (60 mi). References: 1823.
2000 April 6 - Launch Site: Negev. Launch Vehicle: Jericho 1. - Operational Test mission Nation: Israel. Agency: IDF. Apogee: 100 km (60 mi). References: 1603.
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