Zobrazeno 1 - 10
of 48
pro vyhledávání: '"V N Blinov"'
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:
A. S. Tegzhanov, E. Yu. Nosov, V. E. Shcherba, V. N. Blinov, Valery. I. Surikov, A. M. Paramonov
Publikováno v:
Chemical and Petroleum Engineering. 55:733-742
A prototype of a crossheadless hybrid piston power machine is developed based on a basic diagram protected by a patent for an invention. An experimental investigation of the crossheadless machine as well as of a crosshead hybrid piston power machines
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c238254c794a48b077654839caadf690
https://doi.org/10.1007/s10556-020-00687-x
https://doi.org/10.1007/s10556-020-00687-x
Autor:
A. S. Tegzhanov, E.Y. Nosov, V. N. Blinov, Valery. I. Surikov, A. M. Paramonov, V. E. Shcherba
Publikováno v:
Proceedings of Higher Educational Institutions. Маchine Building. :78-85
Piston hybrid power machines combining the functions of a compressor and a pump in one unit have become widespread, with a new class of machines that do not have a crosshead currently under development. A prototype of such a machine was designed and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4fa080df3964eff0543c5364c5921f48
https://doi.org/10.18698/0536-1044-2019-10-78-85
https://doi.org/10.18698/0536-1044-2019-10-78-85
Publikováno v:
Proceedings of Higher Educational Institutions. Маchine Building. :88-95
Currently, one of the main ways to improve the efficiency of piston compressors and volumetric pumps is to combine them into a single unit, called a piston hybrid energy machine. Recently, a new class of crossheadless piston hybrid energy positive di
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7839db9f8290722caf3ed6df326f9d92
https://doi.org/10.18698/0536-1044-2019-9-88-95
https://doi.org/10.18698/0536-1044-2019-9-88-95
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
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4810463a4e223bd6a69b551b5830b3d6