This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 100,000 kg.
Propellants: Lox/Kerosene Country: Russia. Status: Design. Comments: Sled studied in tradeoff studies leading to MAKS. Release conditions: Piggy-back, 290,000 kg, Mach 0.5, zero altitude. Effective velocity gain compared to vertical launch 100 m/s.
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 .