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年12月21日. Last Launch: 2000年04月06日. 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).