| Sanger II-1 |
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Model: Sanger II-1. Gross Mass: 254,000 kg (559,000 lb). Empty Mass: 156,000 kg (343,000 lb). Thrust (vac): 1,499.995 kN (337,212 lbf). Isp: 1,200 sec. Burn time: 6,565 sec. Propellants: Air/LH2. Isp(sl): 3,600 sec. Diameter: 14.00 m (45.00 ft). Span: 41.40 m (135.80 ft). Length: 84.50 m (277.20 ft). Country: Germany. No Engines: 6. Motor: Co-axial turboramjet. Status: Study 1985. Cost $ : 10.000 million. First Flight: 2005. Other designations: EHTV. Releases Horus @M 6.6 @ 37 km altitude @ 3100 km range Used on Launch Vehicles: 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. |