Zobrazeno 1 - 5
of 5
pro vyhledávání: '"S. M. Tsatsuev"'
Publikováno v:
Journal of Applied Mechanics and Technical Physics. 60:80-86
Results of a series of firing tests of two model nozzle extensions made of a carbon-carbon composite material are reported. This material can be used to fabricate nozzle extensions for a large-scale liquid-propellant rocket engine. The tests are perf
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f65a96075068d9e1eca15437be72206c
https://doi.org/10.1134/s0021894419010115
https://doi.org/10.1134/s0021894419010115
Publikováno v:
Thermal Engineering. 59:1062-1067
The method and results of numerical modeling of the radiation-convective heat transfer and thermal state in the systems of multinozzle rocket-engine (RE) assemblies are presented. The method is implemented in a form of a software module entered as th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9b6d5aa9c75e3936f7fdd2e4a25cbb8d
https://doi.org/10.1134/s0040601512140091
https://doi.org/10.1134/s0040601512140091
Autor:
N. N. Volkov, V. V. Mironov, V. V. Koshlakov, V. V. Tlevtsezhev, A. M. Gubertov, S. M. Tsatsuev, L. I. Volkova, N. A. Bratukhin, V. R. Rubinskii, A. V. Pashutov, Ye. A. Antipov
Publikováno v:
Thermal Engineering. 59:1068-1073
The results of the experimental investigation of the physico-chemical processes of interaction, destruction, and ablation of carbon composite materials and oxidation-protective coatings of nozzles of liquid-propellant rocket engines are presented. Th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::02c3b516b9a0a995d2e673bf07a65ee8
https://doi.org/10.1134/s0040601512140042
https://doi.org/10.1134/s0040601512140042
Publikováno v:
Progress in Propulsion Physics.
Computationalandexperimentalinvestigationsofthermochemicalresistance of carbon-ceramic composites in the combustion products of liquidrocketengine(LRE)arepresented. The testswithmodelextensions made of the composite material (CM) were performed. The
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::72b5056049bb103323ad690ff5a13090
https://doi.org/10.1051/eucass/200901659
https://doi.org/10.1051/eucass/200901659
Autor:
N. N. Volkov, S. M. Tsatsuev, V. V. Mironov, L. I. Volkova, V. I. Kondratenko, V. A. Popov, L. B. Treshchalin
Publikováno v:
Progress in Propulsion Physics.
Measuring complex allowing diagnostics of heated-object thermal ¦elds with high resolution was developed. Numerical model was also developed for nozzle tests in vacuum chamber. The model allows simulating the main speci¦c features of the tests. A c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a573df17f0a1682f761527371b05a754
https://doi.org/10.1051/eucass/200901693
https://doi.org/10.1051/eucass/200901693