This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: RSA-3-2, Shavit-2. Used on launch vehicles: RSA-3, Shavit, Shavit 1. Propellants: Solid Thrust(vac): 53,000 kgf. Thrust(vac): 519.00 kN. Isp: 284 sec. Isp (sea level): 220 sec. Burn time: 48 sec. Diameter: 1.3 m. Length: 4.9 m. Chambers: 1. Country: South Africa. Status: Developed -1995. Comments: Built in both Israel and South Africa. Source: Missile exhibit and placards, AF Museum, South Africa.
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Last update 12 March 2001.
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© Mark Wade, 2001 .