Engine Model: RSA-3-1. Propellants: Solid. Thrust(vac): 500.000 kN (112,400 lbf). Isp: 273 sec. Isp (sea level): 230 sec. Burn time: 53 sec. Diameter: 1.30 m (4.20 ft). Length: 5.40 m (17.70 ft). Chambers: 1. Country: South Africa. Status: Out of production. First Flight: 1988. Last Flight: 1990. Flown: 5.00. Built in both Israel and South Africa. Source: Missile exhibit and placards, AF Museum, South Africa.
RSA-3-1 used on Rocket Stages