Zobrazeno 1 - 10
of 32
pro vyhledávání: '"A. I. Lukyanchik"'
Publikováno v:
Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение", Vol 7, Iss 4, Pp 48-55 (2023)
The purpose of the work is to conduct autonomous experimental studies of an resistojet with two autonomous heating elements with a diameter of 4 mm. As a result of experimental studies of the resistojet, the heating dynamics of the micromotor struc
Externí odkaz:
https://doaj.org/article/c48fe3b7a9374617a0a01891ce72b76c
Publikováno v:
Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение", Vol 7, Iss 4, Pp 56-64 (2023)
The paper presents a methodology for constructing a flyby trajectory of a base spacecraft for the purpose of inspecting it using a small spacecraft carried on board and estimating the required characteristic velocity reserves for the flyby maneuver
Externí odkaz:
https://doaj.org/article/b36a1051555448e4a60f682dddc79f8b
Publikováno v:
Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение", Vol 7, Iss 1, Pp 55-60 (2023)
The results of experimental studies on nitrogen with an overpressure of 0,02 MPa resistojet propulsion system of a small spacecraft with a porous structure weighing 45 g and an autonomous heating element with a radius of 3 mm with a power consumpti
Externí odkaz:
https://doaj.org/article/11d349a6ae8e4b9fa821284878a466a3
Publikováno v:
Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение", Vol 5, Iss 4, Pp 75-82 (2021)
In the paper have been discussed nanosetellite propulsion system normalization actual themes, as well their acknowledgement by the testing results. To secure needed survival probability P≥0,995, the propulsion system bottlenecks normalized values
Externí odkaz:
https://doaj.org/article/d98357d087d34f3498081c64ca443943
Publikováno v:
Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение", Vol 3, Iss 2, Pp 95-102 (2019)
A significant number of the main design parameters of the small upper stage for the group launch of small spacecraft with a propulsion system with a displacement fuel supply system determines the relevance of the random search method. The aim of th
Externí odkaz:
https://doaj.org/article/3c5e81b349724b8c882dbd30c66bc346
Publikováno v:
Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение", Vol 2, Iss 3, Pp 26-34 (2018)
A large number of basic design parameters of the ammonia propulsion system makes the task of their search by the method of random search urgent. The aim of the research is to create a mathematical model that is adapted to the chosen method. Mathema
Externí odkaz:
https://doaj.org/article/b03173c72c7f45aeb47ec53cdded2143
Autor:
P. S. Yachmenev, K. I. Zharikov, A. I. Lukyanchik, Viktor Fedyanin, I. S. Vavilov, Pavel Stepen
Publikováno v:
Acta Astronautica. 189:548-558
A method for improving the tactical and technical characteristics of ion thrusters while maintaining the specified electrical characteristics of the power source is proposed. This method is considered on the example of increasing the accelerating vol
Publikováno v:
Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение", Vol 3, Iss 2, Pp 95-102 (2019)
A significant number of the main design parameters of the small upper stage for the group launch of small spacecraft with a propulsion system with a displacement fuel supply system determines the relevance of the random search method. The aim of the
Publikováno v:
Journal of Physics: Conference Series. 2182:012051
The article is devoted to the measurement of the ion beam velocity of an accelerator two-gap ion thruster. A theoretical representation of the physical process of capturing charged particles using a cylindrical sensing element is given. A schematic d
Publikováno v:
Journal of Physics: Conference Series. 2182:012099
This paper presents the results of experimental studies of 15 design versions of capacitive and induction type microwave antennas. As part of the work on the development of an accelerator ion thruster, 32 radiator designs were studied. The research w