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RSA-3-2
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Gross Mass: 10,971 kg (24,186 lb). Empty Mass: 1,771 kg (3,904 lb). Thrust (vac): 476.600 kN (107,144 lbf). Isp: 277 sec. Burn time: 52 sec. Propellants: Solid. Isp(sl): 220 sec. Diameter: 1.30 m (4.20 ft). Span: 1.30 m (4.20 ft). Length: 6.40 m (20.90 ft). Country: South Africa. No Engines: 1. Engine: RSA-3-2. Status: In production. First Flight: 1988. Last Flight: 2004. No Launched: 9. No Failed: 1. Used as: Shavit-2; NEXT-2; RSA-3 - 2. Source: Missile exhibit and placards, AF Museum, South Africa. Empty mass includes 583 kg for payload shroud, guidance, orientation and spin-up platform that positions stage 3 and payload for final orbital insertion burn.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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