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RSA-4-2
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Gross Mass: 11,000 kg (24,000 lb). Empty Mass: 2,000 kg (4,400 lb). Thrust (vac): 470.000 kN (105,660 lbf). Isp: 277 sec. Burn time: 52 sec. Propellants: Solid. 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-4-2. Status: Development ended 1994. Essentially identical to RSA-3 second stage. Includes 1000 kg upper stage avionic section / spin table, which is jettisoned prior to stage three ignition.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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