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- Article name
- MATHEMATICAL MODELS OF SPACE-ROCKET HARDWARE DOWNGOING DESIGN
- Authors
- Filatov A. N., , d0088@samspace.ru, State Research and Production Space-Rocket Center "TsSKB-Progress", Samara, Russia
Kremenetskaya M. E., , mme82@mail.ru, Samara State Aerospace University named after S. P. Korolyov, Samara, Russia
- Keywords
- space-rocket hardware / D&D / downgoing design / mutisequencing / iteration / mathematical model / Admal law / acceleration / Creo Elements/Pro / data management / Windchill PDMLink
- Year
- 2014 Issue 3 Pages 26 - 31
- Code EDN
- Code DOI
- Abstract
- The article deals with mathematical models of iterative process of space-rocket hardware development, that allow assessment of D&D acceleration by their multisequencing and decreasing the number of changes introduced into documentation. Here is given an idea of downgoing design procedure implemented with the help of Creo Elements/Pro (Pro/Engineer) and Windchill PDMLink in TsSKB-Progress. Results of real products analysis are presented here; the analysis was performed on the basis of the developed models and downgoing design.
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