| Skylon |
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Model: Skylon. Gross Mass: 263,000 kg (579,000 lb). Empty Mass: 42,319 kg (93,297 lb). Thrust (vac): 1,300.000 kN (292,200 lbf). Isp: 425 sec. Burn time: 1,200 sec. Propellants: Air/Lox/LH2. Isp(sl): 2,000 sec. Diameter: 6.25 m (20.50 ft). Span: 25.00 m (82.00 ft). Length: 82.00 m (269.00 ft). Country: UK. No Engines: 2. Motor: Sabre. Status: Development ended 1995. Engine thrust, burn time estimated. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. |