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Delta 4 - 2
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Gross Mass: 24,170 kg (53,280 lb). Empty Mass: 2,850 kg (6,280 lb). Thrust (vac): 110.050 kN (24,740 lbf). Isp: 462 sec. Burn time: 850 sec. Propellants: Lox/LH2. Diameter: 2.44 m (8.00 ft). Span: 4.00 m (13.10 ft). Length: 12.00 m (39.00 ft). Country: USA. No Engines: 1. Engine: RL-10B-2. Status: In production. First Flight: 2002. Last Flight: 2006. No Launched: 6. Delta 3 second stage with hydrogen tank stretch.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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