Конференції Національного Авіаційного Університету, AVIATION IN THE XXI-st CENTURY 2018

Розмір шрифту: 
Yuriy Mitikov, Danny Polyakov

Остання редакція: 2018-09-24

Посилання


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  2. Mitikov Y.A., Tatarinov K.A. Analysis of ways to improve the pressurization of propellant tanks for launch vehicles propulsion systems// News of the O. Gonchar DNU: Rocket and space technics – 2017. – №20. – p.50 – 56.
  3. Umanskii S.P. Launch vehicles. Spaceports. Moscow.: Restart+. – 2001. – p.216.
  4. Katorgin B.A. Prospects for the creation of powerful liquid rocket engines / Bulletin of the Russian Academy of Sciences. – 2004. – №3. –  p.499 – 506.
  5. Kluyeva O.G. Creation of a unified heat exchanger for a single-chamber liquid rocket engine//Proceedings of Energomash Corporation. – №25. – 2007.– p.286 – 301.
  6. А.А. Shishkov, B.V. Rumyancev. Gas generators of rocket systems. - M .: Mechanical engineering - 1981. - p. 6-25.
  7. Pressurization systems of the launch vehicles propulsion systems propellant tanks: Patent №108414 Ukraine: MPK B64D 37/00/Mitikov  Y.A. – 2014
  8. Barmin I.V.  Technological objects of the ground infrastructure of rocket and space technology. - M: Poligraphics, 2005 (book 1). - 420 p.
  9. Mitikov Y.A., Andrievskiy M.V. Parameters modeling of the pressurization system of a tank with kerosene by oxygen // Aviation and space technology. - 2013. - No. 1 (98).– p. 85 – 89.
  10. Called by time. The rockets and spacecraft of the Yuzhnoye SDO, under the general editorship of S.N.Konyuhov. – Art-press. – 2004.  – p. 230.
  11. Pressurization system of the propulsion system propellant tanks: Patent №115096 Ukraine: MPK F02k9/50/Mitikov Y.A., Polyakov D.G. – 2017