This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com

astronautix.com R-56 Polyblock

R-56 test model
R-56 test model - R-56 dynamic test model

Credit: © Mark Wade. 12,695 bytes. 119 x 477 pixels.



Family: Tsyklon. Country: Russia. Status: Study 1961. Article Number: 8K68.

One design approach considered for Yangel's R-56 superbooster of the 1960's was a polyblock design limited to rail transport restrictions (4 x 3.8 m diameter stages clustered together). Although a dynamic test model was built and tested at Tsniimash, Yangel finally reached the conclusion that a monoblock design was clearly superior to polyblock versions. Further work on the polyblock design was abandoned. Tsniimash exhibits in its small museum the 1:10 structural simulation model of the 3.8 m diameter polyblock design.


Specifications

Payload: 35,000 kg. to a: 16,000 km ICBM trajectory. Liftoff Thrust: 1,687,500 kgf. Total Mass: 1,165,500 kg. Core Diameter: 7.6 m. Total Length: 51.5 m.



Bibliography:



R-56 test modelR-56 test model - R-56 dynamic test model C

Credit: © Mark Wade. 76,160 bytes. 401 x 576 pixels.



R-56 - detail viewR-56 - detail view - R-56 - detail view of interstage of test model of monster rocket

Credit: © Mark Wade. 19,814 bytes. 198 x 431 pixels.



R-56 test modelR-56 test model - R-56 dynamic test model

Credit: © Mark Wade. 32,660 bytes. 158 x 578 pixels.



R-56, R-26, 63S1R-56, R-26, 63S1 - From left to right, dynamic test models of: R-56 monster launch vehicle; R-26 ICBM; Kosmos 63S1 launch vehicle

Credit: © Mark Wade. 35,088 bytes. 261 x 436 pixels.



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 .