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- Article name
- Using of termostati cally controled honeycomb structures in perspective spacecrafts and antenna systems
- Authors
- KESEL'MAN G.D., , , Federal State Unitary Enterprise "Academician M. F. Reshetnev's research and production association of applied mechanics", Zheleznogorsk, Krasnoyarsky region, Russia
DANILOV E.N., , , Federal State Unitary Enterprise "Academician M. F. Reshetnev's research and production association of applied mechanics", Zheleznogorsk, Krasnoyarsky region, Russia
NAGOVITSIN V.N., , , Federal State Unitary Enterprise "Academician M. F. Reshetnev's research and production association of applied mechanics", Zheleznogorsk, Krasnoyarsky region, Russia
PATRAEV E.V., , , Federal State Unitary Enterprise "Academician M. F. Reshetnev's research and production association of applied mechanics", Zheleznogorsk, Krasnoyarsky region, Russia
GRYAZNOV V.N., , , Federal State Unitary Enterprise "Academician M. F. Reshetnev's research and production association of applied mechanics", Zheleznogorsk, Krasnoyarsky region, Russia
- Keywords
- Year
- 2005 Issue 3 Pages 10 - 13
- Code EDN
- Code DOI
- Abstract
- Using of honeycomb structures in perspective spacecrafts is substantiated. Advantages of honeycomb structures in contrast with the other structures are shown. Elements and used materials are determined. Results of analysis of deflected mode of honeycomb structures with use of finite-elements models are given.
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