| KSR-3 |
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Model: KSR-3. Gross Mass: 5,000 kg (11,000 lb). Empty Mass: 700 kg (1,540 lb). Thrust (vac): 122.500 kN (27,539 lbf). Isp: 280 sec. Burn time: 95 sec. Propellants: Lox/Kerosene. Isp(sl): 240 sec. Diameter: 1.00 m (3.20 ft). Span: 1.00 m (3.20 ft). Length: 9.60 m (31.40 ft). Country: Korea South. No Engines: 1. Motor: KSR-3. Status: In development. First Flight: 2002. Last Flight: 2002. No Launched: 1. All values except thrust estimated. Used on Launch Vehicles:
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