astronautix.com | R-56 Polyblock |
![]() |
R-56 test model - R-56 dynamic test model Credit: © Mark Wade. 12,695 bytes. 119 x 477 pixels. |
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.
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.
![]() | R-56 test model - R-56 dynamic test model C Credit: © Mark Wade. 76,160 bytes. 401 x 576 pixels. |
![]() | R-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 model - R-56 dynamic test model Credit: © Mark Wade. 32,660 bytes. 158 x 578 pixels. |
![]() | R-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. |