TECHNICAL MECHANICS
ISSN (Print): 1561-9184, ISSN (Online): 2616-6380

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UDC 629.7+531.3+532.6

Technical mechanics, 2016, 4, 50 - 61

INCREASE IN TARGET-ORIENTED EFFICIENCY OF SPACE MEDIUM-SIZED ROCKET: ADVANCED LINES FOR UPDATING

V. V. Gorbuntsov, A. N. Zavoloka, N. F. Sviridenko

      ABOUT THE AUTHORS

V. V. Gorbuntsov
Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine
Ukraine

A. N. Zavoloka
Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine
Ukraine

N. F. Sviridenko
Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine
Ukraine

      ABSTRACT

      Advanced lines for updating the space medium-sized carrier rockets (SMSCR) are offered increasing their target-oriented efficiency in an extended operational range. To attain this, untapped internal reserves are considered based on the active control of current state of the SMSCR elastodeforming body and a hydrodynamic situation in its fuel tanks with the use of SMSCR-born equipment. The terminal control of the angular motion of the first stage of the SMSCR can also be employed taking into account limitations of the control parameters of the flight. The energetically optimal algorithm for launching and servicing the discrete payload by the space stage of the SMSCR is realized using the algebraic methods of the discrete-event simulation. Pdf (English)







      KEYWORDS

space rocket, space stage, monitoring current state, elastodeforming body, terminal control, fuel feed system, free gas inclusions, pressurization system, turbulent vortex rings, discrete-event simulation.

      FULL TEXT:

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Copyright (©) 2016 V. V. Gorbuntsov, A. N. Zavoloka, N. F. Sviridenko

Copyright © 2014-2018 Technical mechanics


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