This page no longer updated from 31 October 2001. Latest version can be found at UR-200 Stage 2

RD-0205 8D46
RD-0205 8D46
RD-0205 8D46 on stage 8S816 (UR-200)

Credit: © Mark Wade. 45,159 bytes. 576 x 400 pixels.

Gross Mass: 25,810 kg. Empty Mass: 2,400 kg. Thrust (vac): 62,500 kgf. Isp: 322 sec. Burn time: 113 sec. Propellants: N2O4/UDMH Diameter: 2.2 m. Span: 2.2 m. Length: 10.0 m. Country: Russia. No Engines: 1. RD-0205 Status: Hardware. Other designations: 8K81 Stage 2. Comments: Tsniimash has 1:10 structural simulation model. Developed 1960-1965. Orevo has sectioned hardware. All data accurate except empty mass prorated between first and second stages.
Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .