This page no longer updated from 31 October 2001. Latest version can be found at LeoLink LK-1

Family: Miscellany. Country: Israel. Status: Development.

Satellite launcher derived from planned Israeli Shavit-2 launch vehicle, but with rocket motors and major components built in USA to qualify for US contracts.


LEO Payload: 550 kg. to: 200 km Orbit. at: 0.0 degrees. Payload: 415 kg. to a: Sun synchronous, 800 km, 98.5 deg orbital trajectory. Liftoff Thrust: 60,000 kgf. Total Mass: 30,500 kg. Core Diameter: 1.4 m. Total Length: 20.9 m. Launch Price $: 15.00 million. in 1999 price dollars.


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Last update 12 March 2001.
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© Mark Wade, 2001 .