Zobrazeno 1 - 10
of 124
pro vyhledávání: '"Yuzhnoye State Design Office"'
Autor:
D.K. Mozgovoy, K.G. Belousov, Yangel Yuzhnoye State Design Office, Dnipro, Ukraine, V.S. Khoroshylov, A.L. Makarov, V.M. Popel, D.N. Svinarenko, Yuzhnoye State Design Office, Dnipro, Ukraine
Publikováno v:
Kosmìčna nauka ì tehnologìâ. 27:42-53
The results of testing the developed techniques for automatized recognition of vegetation and water bodies on the urban territory by multispectral images from the Jilin-1А satellite are given.The research included automatized recognition of vegetati
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f8cef2cf3ebcd0dfcf48c0506095d248
https://doi.org/10.15407/knit2021.04.042
https://doi.org/10.15407/knit2021.04.042
Publikováno v:
Technical mechanics. 2021:83-98
The aim of this work is to develop a methodological approach to the development of a unified, common for all developers, computer-aided branch procedure for spacecraft development cost estimation based on a spacecraft cost model and practical recomme
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4ccd4e513afac306bec377cde991bfa9
https://doi.org/10.15407/itm2021.03.083
https://doi.org/10.15407/itm2021.03.083
Publikováno v:
Technical mechanics. 2021:37-47
Up-to-date multiple launch rocket systems (MLRSs) are adopted by many countries of the world, and they are an effective weapon against dispersed multiple targets. Developing and upgrading MLRSs calls for estimating their efficiency with the aim to se
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::277b80c61cb9b4ee1a241ce9ca29d0f2
https://doi.org/10.15407/itm2021.03.037
https://doi.org/10.15407/itm2021.03.037
Autor:
N.V. Khoriak, Yuzhnoye State Design Office, Dnipro, Ukraine, D.V. Klimenko, S.I. Dolgopolov, M.A. Degtyarev, Yangel Yuzhnoye State Design Office, Dnipro, Ukraine, L.A. Silkin, O.V. Pylypenko, A.D. Nikolaev, I.D. Bashliy
Publikováno v:
Kosmìčna nauka ì tehnologìâ. 26:3-20
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::241b92f9bc77326bf7a239e514de3283
https://doi.org/10.15407/knit2020.04.003
https://doi.org/10.15407/knit2020.04.003
Autor:
D.V. Klymenko, Yangel Yuzhnoye State Design Office, Dnipro, Ukraine, L.D. Levytina, A.P. Dzyuba, D.A. Cherenkov, Yuzhnoye State Design Office, Dnipro, Ukraine, V.N. Sirenko
Publikováno v:
Kosmìčna nauka ì tehnologìâ. 26:28-37
We considered the problem of weight optimization of parameters of multi-layer composite shell produced by the method of continuous cross-winding under axisymmetric loading. Shell layers are placed symmetrically relative to the middle surface. The ang
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::68f5cb8f534e91cd3724fcb46d395d49
https://doi.org/10.15407/knit2020.05.028
https://doi.org/10.15407/knit2020.05.028
Publikováno v:
Journal of Mechanical Engineering, Vol 24, Iss 2, Pp 16-23 (2021)
FDM 3D printed honeycombs are investigated. A honeycomb is composed of regular hexagonal cells. A honeycomb is 3D printed so that the fused filament runs along the walls of its cells. We emphasize that the thickness of these walls is one or two times
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7d189c17805eb9d0f637aa7f4462b227
https://doi.org/10.15407/pmach2021.02.016
https://doi.org/10.15407/pmach2021.02.016
Publikováno v:
Technical mechanics. 2021:68-76
In integrated launch vehicles, one of the systems responsible for successful launch preparation and support is a ground thermal conditioning system supplying low-pressure thermostatic air to the “dry” compartments and head blocks of a launch vehi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::da0810133a1a1ad8062b75f6817c3abf
https://doi.org/10.15407/itm2021.01.068
https://doi.org/10.15407/itm2021.01.068
Publikováno v:
Technical mechanics. 2021:92-100
Additive manufacturing is very promising for aerospace engineering and aircraft construction. Using these technologies, light structures with preset strength properties can be made. For lack of tables of the mechanical properties of materials made by
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::772cf48a5880c15eb9605ec2595265be
https://doi.org/10.15407/itm2021.01.092
https://doi.org/10.15407/itm2021.01.092
Autor:
Yuzhnoye State Design Office, E. L. Hart, Dmitriy V. Klimenko, V. S. Hudramovich, Vladimir N. Sirenko
Publikováno v:
Technical mechanics. 2021:3-15
Shell structures provide a compromise between strength and mass, which motivates their use in rocket and space hardware (RSH). High and long-term loads cause plastic and creep deformations in structural elements. RSH structures feature inhomogeneity:
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::05ff6d88131e08db29f37680ffd137af
https://doi.org/10.15407/itm2021.01.003
https://doi.org/10.15407/itm2021.01.003
Autor:
A.S. Bilous, Yangel Yuzhnoye State Design Office, Dnipro, Ukraine, M.A. Degtyarev, D.V. Akimov, K.V. Avramov
Publikováno v:
Kosmìčna nauka ì tehnologìâ. 27:3-10
The thermal strength of the retention compartment is calculated to analyze the possibility of multiple use for a rocket start. The transient heat field of the retention compartment, which is induced by the interaction of the exhaust gas with the rete
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::902f8affbbd28138f57d00d477bed69b
https://doi.org/10.15407/knit2021.04.003
https://doi.org/10.15407/knit2021.04.003