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Information × Registration Number 0310U002631, 0106U007065 , R & D reports Title Participation in autonomous development of the board section of the high-pressure thermostatic control system of the Zenith-2SLB with presentation of measuring technique popup.stage_title Участь в автономному відпрацюванні бортової частини системи термостатування високим тиском РКП "Зеніт-2SLБ" з наданням вимірювальної техніки Head Tymoshenko V. I., Registration Date 17-05-2010 Organization Institute of Technical Mechanics of NASU and NSAU popup.description2 The research subjects are measurement means of the on-board section for the thermostatic control high-pressure system of the Zenith-2SLB LV. The research goal is to determine experimentally the calibration characteristics of semi-conductor hot-wire transducers in a range of low air velocities at simulation of the thermostatic-controlling air flow using a test design of a noise fairing. The experimental method is used. The program and the procedure for calibrating the TS-2 semi-conductor hot-wire velocity transducers in the wind tunnel of the Dnepropetrovsk National University are proposed. These transducers are designed to measure the air velocity under autonomic tests of the thermostatic control system of the Zenith-2SLB LV section using a high-pressure air of 0.5-27 m/s. The calibration dependences for 20 TC-2 velocity transducers are derived using various subranges of variations in the air velocity. The results obtained will be used in the autonomic development of the thermostatic control high-pressure air section of the Zenith-2SLB LV spacecraft. The economic importance of the research is determined by programs of the development of priority lines of the Ukraine's industry. The application field - rocket-space mechanics. Product Description popup.authors Книшенко Ю.В. Осадчій О. В. Пластун В.І. Тимошенко В. І. popup.nrat_date 2020-04-02 Close