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CLV Stage 2
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Gross Mass: 160,000 kg (350,000 lb). Empty Mass: 16,000 kg (35,000 lb). Thrust (vac): 2,333.000 kN (524,479 lbf). Isp: 465 sec. Burn time: 270 sec. Propellants: Lox/LH2. Diameter: 5.50 m (18.00 ft). Span: 5.50 m (18.00 ft). Length: 32.00 m (104.00 ft). Country: USA. No Engines: 1. Engine: SSME. Status: Study 2005. Second stage proposed by NASA for launch of CEV into low earth orbit. All masses estimated.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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