Investigation of force and thermal loading of jet deflectors of launch complexes of space rockets during the work of water supply systems

Автор: Sinilshchikov B.E., Sinilshchikov V.B.

Журнал: Космические аппараты и технологии.

Рубрика: Ракетно-космическая техника

Статья в выпуске: 2 (20), 2017 года.

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In the most of modern launch complexes of space rockets the water supply systems are used to defend the surfaces acted directly upon by high-temperature jet flows from melting. The paper presents the estimation for parameters of force and heat loads of jet deflector during the work of intra-jet and extrajet water supply systems. The method of numerical simulation for two-phase gas-droplet flows is used. The description of a mathematical model is given. For description of gas flow the Navier-Stokes equations completed with an algebraic model of turbulence are applied, this model being similar to the Prandtl one but taking into account the influence of a droplet phase. Thermodynamic parameters are determined by the model of ideal gas for a mechanical mixture of three components: combustion products, atmospheric air, and vapor (steam) formed as a result of water evaporation. The flow of a droplet phase is calculated on the base of continual approach with using the elements of trajectory approach...

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Rocket engine, jet, water supply, heat flows, evaporation, jet deflector, breakup

Короткий адрес: https://sciup.org/14117393

IDR: 14117393

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