Two different complex problems arising during spacecraft design are discussed in this paper. One problem is a definition of impulse for a safety separation of a parachute container lid. Another problem is defining a shock-wave interaction on the spacecraft at turning on emergency rescue system. Both problem are very hard and expensive for solving by experimental methods, and RSC Energia gets here all benefits of numerical simulation by using CFD code FlowVision.
Aksenov A.A., Dyadkin А.А., Rybak S.P., Simakova T.V., TESIS Ltd, Moscow, Russia, JSV «RSC Energia» Korolev, Russia
29th Congress of the International Council of the Aeronautical Sciences, St. Petersburg, Russia, September 7-12, 2014, Page 1/5