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Jericho-1
Part of Jericho Family
Israeli short range ballistic missile. Follow-on version differed from original French-derived Jericho. Probably used a single 4500 kg solid-propellant motor.

AKA: Jericho 1. Status: Active. First Launch: 1990-12-21. Last Launch: 2000-04-06. Number: 3 . Payload: 500 kg (1,100 lb). Gross mass: 4,500 kg (9,900 lb). Height: 10.06 m (33.00 ft). Diameter: 1.01 m (3.31 ft). Span: 1.01 m (3.31 ft). Location: Be'er Yaakov, Israel. Apogee: 100 km (60 mi).

Maximum range: 480 km (290 mi). Boost Propulsion: Solid rocket.



Family: short range ballistic. Country: Israel. Launch Sites: Negev. Stages: Jericho-1-1. Agency: IAI.

1990 December 21 - . Launch Site: Negev. LV Family: Jericho. Launch Vehicle: Jericho-1.
  • Operational test - . Nation: Israel. Agency: IDF. Apogee: 100 km (60 mi).

1991 October 30 - . Launch Site: Negev. LV Family: Jericho. Launch Vehicle: Jericho-1.
  • Operational test - . Nation: Israel. Agency: IDF. Apogee: 100 km (60 mi).

2000 April 6 - . Launch Site: Negev. LV Family: Jericho. Launch Vehicle: Jericho-1.
  • Operational test - . Nation: Israel. Agency: IDF. Apogee: 100 km (60 mi).


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