LeoLink LK-2

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LeoLink LK-2

Part of Jericho

Israeli all-solid orbital launch vehicle. As Leolink LK-1, but with a Castor-120 motor as the first stage.

Status: Development ended 2002. Payload: 1,550 kg (3,410 lb). Thrust: 1,450.00 kN (325,970 lbf). Gross mass: 70,000 kg (154,000 lb). Height: 26.40 m (86.60 ft). Diameter: 2.30 m (7.50 ft). Apogee: 200 km (120 mi).

LEO Payload: 1,550 kg (3,410 lb) to a 200 km orbit. Payload: 1,200 kg (2,600 lb) to a 800 km SSO. Launch Price $: 20.000 million in 1999 dollars.

Family: all-solid, orbital launch vehicle. Country: Israel. Stages: LK-1 engine. Agency: IAI.

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