This page no longer updated from 31 October 2001. Latest version can be found at Burlak Stage 2

Gross Mass: 9,400 kg. Empty Mass: 900 kg. Thrust (vac): 10,000 kgf. Isp: 330 sec. Burn time: 275 sec. Propellants: N2O4/UDMH Isp(sl): 230 sec. Diameter: 1.6 m. Span: 1.6 m. Length: 5.5 m. Country: Russia. No Engines: 1. Burlak Stage 2 Status: Hardware. Comments: Masses, thrust, specific impulse estimated based on total vehicle mass of 28.5 tonnes and first stage burn time of 140 seconds. Air launched from Tu-160 at 13,500 m, Mach 1.7 release conditions.
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 .