Zobrazeno 1 - 10
of 15
pro vyhledávání: '"ракета-носій"'
Autor:
Oleksandr Minai
Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 1, Pp 43-55 (2024)
The subject of this study is the corrosion processes that occur in the fuel tanks of spacecraft with a long service life, the engines of which operate on chemically aggressive fuel components (FC): nitrogen tetroxide (NT) and asymmetric dimethylhydra
Externí odkaz:
https://doaj.org/article/7a9edf28883b46c182f61819299f9574
Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 5, Pp 60-68 (2021)
The object of the article is the movement of an ultra-light class liquid-propellant launch vehicle in near-earth space. The subject of the research is the accuracy of launching a spacecraft by a launch vehicle. The article studies the effect of error
Externí odkaz:
https://doaj.org/article/d7928c13be4d42c3ba39c32b68d8fbb9
Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 2, Pp 22-25 (2017)
This paper concerns the problem of liquid propellant launch vehicles delivery to the launch center. The variants of launch vehicles transportation using rail, road and air transport were considered. The key problems of transportation using the aircra
Externí odkaz:
https://doaj.org/article/c24629a5bbdd4b07b87db74a17c60505
The article reviews the contribution of Ukrainian enterprises to the development of the rocket and space industry. The most important part of a space or combat ballistic missile is the control system (CS), on which the success of its application depe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______3033::151ecbedd27b6121e8311c0ad8768f14
http://repository.kpi.kharkov.ua/handle/KhPI-Press/54173
http://repository.kpi.kharkov.ua/handle/KhPI-Press/54173
Publikováno v:
Проблемы машиностроения; Том 23, № 3 (2020); 27-36
Проблеми машинобудування; Том 23, № 3 (2020); 27-36
Journal of Mechanical Engineering; Том 23, № 3 (2020); 27-36
Проблеми машинобудування; Том 23, № 3 (2020); 27-36
Journal of Mechanical Engineering; Том 23, № 3 (2020); 27-36
A technique has been developed for reducing the material intensity of highly stressed tail sections of launch vehicles, taking into account strength and stability constraints as well as technological requirements. A cylindrical longitudinally and tra
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=scientific_p::f8baf765bb35826563fdbea241b0c52d
http://journals.uran.ua/jme/article/view/213127
http://journals.uran.ua/jme/article/view/213127
Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 2, Pp 22-25 (2017)
This paper concerns the problem of liquid propellant launch vehicles delivery to the launch center. The variants of launch vehicles transportation using rail, road and air transport were considered. The key problems of transportation using the aircra
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doajarticles::1f277b6e9f941b27068134ad4d40e2f3
http://nti.khai.edu/ojs/index.php/aktt/article/view/482
http://nti.khai.edu/ojs/index.php/aktt/article/view/482
ОЦІНКА МОЖЛИВОСТЕЙ ЗАСТОСУВАННЯ ТВЕРДИХ ВУГЛЕВОДНІВ В АВТОФАЖНИХ ДВИГУНАХ РАКЕТ-НОСІЇВ ЛЕГКОГО КЛАСУ
Publikováno v:
Journal of Chemistry and Technologies; Том 27, № 1 (2019): Journal of Chemistry and Technologies; 58-64
The perspective way of reducing the cost of transport space operations is analyzed. It is shown that using propellant tanks polyethylene covers as fuel is the most effective way to reduce the cost of launching a satellite to low near-Earth orbits. Th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=scientific_p::cab068c44bea1c2d1f4f9b79ff5abbab
http://chemistry.dnu.dp.ua/article/view/081906
http://chemistry.dnu.dp.ua/article/view/081906
Publikováno v:
Journal of Chemistry and Technologies; Vol 27, No 1 (2019): Journal of Chemistry and Technologies; 58-64
The perspective way of reducing the cost of transport space operations is analyzed. It is shown that using propellant tanks polyethylene covers as fuel is the most effective way to reduce the cost of launching a satellite to low near-Earth orbits. Th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ee04ff05e2b4ca011cdce08a12023b0f
http://chemistry.dnu.dp.ua/article/view/081906
http://chemistry.dnu.dp.ua/article/view/081906
Publikováno v:
Industrial Gases; № 4 (2015): ; 66-72
Технические газы; № 4 (2015): Технические газы; 66-72
Технічні гази; № 4 (2015): ; 66-72
Технические газы; № 4 (2015): Технические газы; 66-72
Технічні гази; № 4 (2015): ; 66-72
При подготовке к пуску космических ракет-носителей «Ангара» возникает необходимость в термостатировании их отсеков, отдельных элемент
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=scientific_p::c74054a5719e3775f9d4dd720bb6c259
http://journals.uran.ua/IndustrialGases/article/view/0791
http://journals.uran.ua/IndustrialGases/article/view/0791