X-30

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Model: X-30. Gross Mass: 140,000 kg (300,000 lb). Empty Mass: 60,000 kg (132,000 lb). Thrust (vac): 1,370.000 kN (307,980 lbf). Isp: 1,550 sec. Burn time: 886 sec. Propellants: Air/Slush LH2. Isp(sl): 1,550 sec. Diameter: 16.00 m (52.00 ft). Span: 36.00 m (118.00 ft). Length: 80.00 m (262.00 ft). Country: USA. No Engines: 1. Motor: Scramjet. Status: Development ended 1990. Cost $ : 3,000.000 million. First Flight: 2001. Other designations: NASP (National Aerospace Plane); Orient Express. Used on Launch Vehicles: X-30. 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.