Veskov Е. V., Nazarenko Е. P., Sedykh I. V., Shevchenko B. А.
Yangel Yuzhnoye State Design Office, Dnipro, Ukraine
Kosm. teh. Raket. vooruž. 2017 (2); 77-82
Two design options of manifold and dividing valve are considered, the loss calculation by analytical and numerical methods has been made. Based on the calculation results, the optimal design option has been selected. The calculation correctness is confirmed as a result of development tests of the design.