This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 254,000 kg.
Empty Mass: 156,000 kg. Thrust (vac): 152,957 kgf. Isp: 1,200 sec. Burn time: 6,565 sec. Propellants: Air/LH2 Isp(sl): 3,600 sec. Diameter: 14.0 m. Span: 41.4 m. Length: 84.5 m. Country: Germany. No Engines: 6. Co-axial turboramjet Status: Study. Other designations: EHTV. Comments: Releases Horus @M 6.6 @ 37 km altitude @ 3100 km range.
Back to Index
Last update 12 March 2001.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .