Engine Model: RSA-3-2. Propellants: Solid. Thrust(vac): 519.000 kN (116,675 lbf). Isp: 284 sec. Isp (sea level): 220 sec. Burn time: 48 sec. Diameter: 1.30 m (4.20 ft). Length: 4.90 m (16.00 ft). Chambers: 1. Country: South Africa. Status: In production. First Flight: 1988. Last Flight: 2004. Flown: 9.00. Built in both Israel and South Africa. Source: Missile exhibit and placards, AF Museum, South Africa.
RSA-3-2 used on Rocket Stages