Kharchenko M. Synthesis of rational design and technological solutions carbon fiber shapes and sizes of stable structures for space purposes.

Object - processes of design and production dimension stable structures for orbital aircraft; goal - to improve functional properties and mass efficiency of the structures used in spacecraft by developing and implementing a series of rational design and technology solutions based on the use of sandwich panels; research methods - analytical models of composite mechanics, finite element method, analytical models, theory of elasticity orthotropic composite, theoretical bases of obtaining technology the carbon-carbon composites, experimental development research; practical outcomes - the establishment of relations and regularities formation of physic-mechanical properties and tension structures, developed new constructive and technological solutions of main reinforcement carbon fiber cell aggregates, and method for its manufacture; the scientific novelty of the research direction in the theory of optimal design honeycomb construction; the results introduced in the Yuzhnoye State Design Office, JSC "UkrNIITM", Oles Honchar Dnipropetrovsk national university, National Aerospace University - Kharkov Aviation Institute; branch - rocketry.