Yepifanov C. Parametrical identification of power installations of space vehicles with the two-phase heat-carrier

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0404U002833

Thesis Registration Form

0404U002833.pdf

Applicant for

Specialization

  • 05.07.05 - Двигуни та енергоустановки літальних апаратів

04-06-2004

Specialized Academic Board

Д64.062.02

Essay

The thesis is devoted to solution of spacecraft power plants working charac-teristics determination task for spacecraft power plants with high technical measures efficiency design. Developed mathematical model parameters determination method is used for definition of the heat transfer intensity in conditions of mircrogravity. As a result of identification the ratio describing dependence of heat transfer coefficients during condensation on thread-like surface from state parameters in conditions of micro-gravity is received.

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Files

ДИССЕРТАЦИЯ-Введение.doc

ДИССЕРТАЦИЯ-Выводы.doc

ДИССЕРТАЦИЯ-Глава_ 4.doc

ДИССЕРТАЦИЯ-Глава_1.doc

ДИССЕРТАЦИЯ-Глава_2.doc

ДИССЕРТАЦИЯ-Главав_ 3.doc

ДИССЕРТАЦИЯ-СПИСОК ИСПОЛЬЗОВАННЫХ ИСТОЧНИКОВ.doc

ДИССЕРТАЦИЯ-Содержание.doc

ДИССЕРТАЦИЯ-перечень_усл_обозн.doc

ДИССЕРТАЦИЯ-титульный.doc

Укр-ukr_ref_XAI (title).doc

Укр-В печать.doc

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