This page no longer updated from 31 October 2001. Latest version can be found at RSA-3-1

Used on stages: RSA-3-1, Shavit-1. Used on launch vehicles: RSA-3, Shavit. Propellants: Solid Thrust(vac): 51,000 kgf. Thrust(vac): 500.00 kN. Isp: 273 sec. Isp (sea level): 230 sec. Burn time: 53 sec. Diameter: 1.3 m. Length: 5.4 m. Chambers: 1. Country: South Africa. Status: Out of Production. 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 .