This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 30,710 kg.
Empty Mass: 3,490 kg. Thrust (vac): 11,222 kgf. Isp: 462 sec. Burn time: 1,125 sec. Propellants: Lox/LH2 Diameter: 2.4 m. Span: 5.0 m. Length: 12.0 m. Country: USA. No Engines: 1. RL-10B-2 Status: Development. Comments: Delta 4 second stage with hydrogen tank increased to 5.1 m diameter.
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 .