Analysis of Temperature Field in the Transport Compartment of the Launch Vehicle
| dc.contributor.author | Biliaiev, Mykola M. | en |
| dc.contributor.author | Rusakova, Tetiana I. | en |
| dc.contributor.author | Biliaieva, Viktoriia V. | en |
| dc.contributor.author | Kozachyna, Vitalii A. | en |
| dc.contributor.author | Berlov, Oleksandr V. | en |
| dc.contributor.author | Semenenko, Pavlo | en |
| dc.date.accessioned | 2023-03-08T08:45:18Z | |
| dc.date.available | 2023-03-08T08:45:18Z | |
| dc.date.issued | 2022 | |
| dc.description | M. Biliaiev: ORCID 0000-0002-1531-7882, V. Biliaieva: ORCID 0000-0003-2399-3124, V. Kozachyna: ORCID 0000-0002-6894-5532; O. Berlov: ORCID 0000-0002-7442-0548; T. Rusakova: ORCID 0000-0001-5526-3578 | |
| dc.description.abstract | ENG: The development of satellite linkage systems is based on the satellite’s transportation in space. The transportation of a satellite into orbit is carried out by a launch vehicle. The satellite is located in the transport compartment inside the main fairing. At the stage of the pre-launch preparation, it is necessary to fulfill very strict environment conditions inside the main fairing. Namely, it is very important to predict temperature field in the transport compartment inside the main fairing during its forced ventilation at the stage of pre-launch preparation. To calculate the temperature field formed by the ventilation of the transport compartment and release of heat from different elements of the satellite, the energy equation was used. This equation took into account the intensity of heat release from different parts of satellite, air flow pattern over the satellite, heat transfer in the transport compartment. The non-uniform field of the air flow velocity in the transport compartment was calculated on the basis of the potential flow model. The finite difference schemes were used for numerical integration of modeling equations. The computer code has been developed that implements the proposed numerical model. The results of computational experiments to estimate the temperature regime in the main fairing of the launch vehicle for different satellites is presented. | en |
| dc.identifier.citation | Biliaiev M., Rusakova T., Biliaieva V., Kozachyna V., Berlov O., Semenenko P. Analysis of Temperature Field in the Transport Compartment of the Launch Vehicle. Transport Means 2022 : Proc. of the 26th Intern. Sci. Conf. (05–07 Oct., 2022, Kaunas, Lithuania). Kaunas, 2022. Pt. I. P 122–127. | en |
| dc.identifier.uri | https://crust.ust.edu.ua/handle/123456789/16592 | |
| dc.identifier.uri | https://transportmeans.ktu.edu/transport-means-2022/ | |
| dc.language.iso | en | |
| dc.publisher | Kaunas University of Technology, Kaunas | en |
| dc.subject | main fairing | en |
| dc.subject | satellite | en |
| dc.subject | stage of pre-launch preparation | en |
| dc.subject | transport compartment | en |
| dc.subject | temperature field | en |
| dc.subject | КГВ | uk_UA |
| dc.title | Analysis of Temperature Field in the Transport Compartment of the Launch Vehicle | en |
| dc.type | Article | en |