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UDC 629.764 : 662.25+577.4
Technical mechanics, 2017, 1, 3 - 14
DETERMINATION OF INITIAL CHARACTERISTICS OF FUEL COMPONENTS
DROPLET CLOUD DERIVED FROM IN-FLIGHT EXPLOSION OF CARRIER
ROCKET
DOI:
https://doi.org/10.15407/itm2017.01.003
Pylypenko V. V., Gorbutsov V. V., Zavoloka A. N., Sviridenko N. F.
Pylypenko V. V.
Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine
Ukraine
Gorbutsov V. V.
Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine
Ukraine
Zavoloka A. N.
Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine
Ukraine
Sviridenko N. F.
Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine
Ukraine
The methodical approach to the determination of the initial kinematics and geometrical characteristics of
the fuel components droplet cloud derived from the liquid-propellant carrier rocket (CR) explosion at the atmos- pheric trajectory leg is developed. The phenomenological analogy of the transient-load damage processes in the
fractured solids and a mass of a gas-saturated cavitation liquid is taken as a basis of the approach. The droplet
cloud characteristics obtained by this means can be used as the reference data for calculating the subsequent
transformation of the cloud when it moves in the gravitation field taking into account heat-mass exchange with an
atmosphere, as well as for estimating the ecological risks in the ground area of the CR fallout.
carrier rocket, explosion, gas-saturated fuel components, fragmentation,
dispersion, droplet cloud
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DOI:
https://doi.org/10.15407/itm2017.01.003
Copyright (©) 2017 V. V. Pylypenko, V. V. Gorbutsov, A. N. Zavoloka, N. F. Sviridenko
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