Standard

Time-saving method of orbital thermal regime calculations of nanosatellites as exemplified by a 3U CubeSat. / Gorev, Vasily; Prokopyev, Vitaly; Prokopyev, Yury и др.

в: MATEC Web of Conferences, Том 158, 01012, 19.03.2018.

Результаты исследований: Научные публикации в периодических изданиях › статья по материалам конференции › Рецензирование

Harvard

Gorev, V, Prokopyev, V, Prokopyev, Y & Sidorchuk, A 2018, 'Time-saving method of orbital thermal regime calculations of nanosatellites as exemplified by a 3U CubeSat', MATEC Web of Conferences, Том. 158, 01012. https://doi.org/10.1051/matecconf/201815801012

APA

Gorev, V., Prokopyev, V., Prokopyev, Y., & Sidorchuk, A. (2018). Time-saving method of orbital thermal regime calculations of nanosatellites as exemplified by a 3U CubeSat. MATEC Web of Conferences, 158, [01012]. https://doi.org/10.1051/matecconf/201815801012

Vancouver

Gorev V, Prokopyev V, Prokopyev Y, Sidorchuk A. Time-saving method of orbital thermal regime calculations of nanosatellites as exemplified by a 3U CubeSat. MATEC Web of Conferences. 2018 март 19;158:01012. doi: 10.1051/matecconf/201815801012

Author

Gorev, Vasily ; Prokopyev, Vitaly ; Prokopyev, Yury и др. / Time-saving method of orbital thermal regime calculations of nanosatellites as exemplified by a 3U CubeSat. в: MATEC Web of Conferences. 2018 ; Том 158.

BibTeX

@article{a5d048059ff94767a6a1994f4589ede3,
title = "Time-saving method of orbital thermal regime calculations of nanosatellites as exemplified by a 3U CubeSat",
abstract = "A time-saving approach to perform technical calculations of thermal conditions of orbital motion of 3U CubeSat nanosatellite was applied, which made it possible to make the thermal calculations of a satellite with simple structure geometry using MatLab and SolidWorks Simulation. Passive thermal regulation facilities are sufficient for a 3U CubeSat to provide thermal conductivity of the case's structural elements and to remove heat from the lighted surface and internal components to the satellite's shadowed surface. Application of spectrally selective coatings allows narrowing the range of surface temperatures of 3U CubeSat.",
author = "Vasily Gorev and Vitaly Prokopyev and Yury Prokopyev and Alexey Sidorchuk",
year = "2018",
month = mar,
day = "19",
doi = "10.1051/matecconf/201815801012",
language = "English",
volume = "158",
journal = "MATEC Web of Conferences",
issn = "2261-236X",
publisher = "EDP Sciences",
note = "6th International Forum for Young Scientists on Space Engineering 2018 ; Conference date: 26-04-2018 Through 28-04-2018",

}

RIS

TY - JOUR

T1 - Time-saving method of orbital thermal regime calculations of nanosatellites as exemplified by a 3U CubeSat

AU - Gorev, Vasily

AU - Prokopyev, Vitaly

AU - Prokopyev, Yury

AU - Sidorchuk, Alexey

PY - 2018/3/19

Y1 - 2018/3/19

N2 - A time-saving approach to perform technical calculations of thermal conditions of orbital motion of 3U CubeSat nanosatellite was applied, which made it possible to make the thermal calculations of a satellite with simple structure geometry using MatLab and SolidWorks Simulation. Passive thermal regulation facilities are sufficient for a 3U CubeSat to provide thermal conductivity of the case's structural elements and to remove heat from the lighted surface and internal components to the satellite's shadowed surface. Application of spectrally selective coatings allows narrowing the range of surface temperatures of 3U CubeSat.

AB - A time-saving approach to perform technical calculations of thermal conditions of orbital motion of 3U CubeSat nanosatellite was applied, which made it possible to make the thermal calculations of a satellite with simple structure geometry using MatLab and SolidWorks Simulation. Passive thermal regulation facilities are sufficient for a 3U CubeSat to provide thermal conductivity of the case's structural elements and to remove heat from the lighted surface and internal components to the satellite's shadowed surface. Application of spectrally selective coatings allows narrowing the range of surface temperatures of 3U CubeSat.

UR - http://www.scopus.com/inward/record.url?scp=85047761775&partnerID=8YFLogxK

U2 - 10.1051/matecconf/201815801012

DO - 10.1051/matecconf/201815801012

M3 - Conference article

AN - SCOPUS:85047761775

VL - 158

JO - MATEC Web of Conferences

JF - MATEC Web of Conferences

SN - 2261-236X

M1 - 01012

T2 - 6th International Forum for Young Scientists on Space Engineering 2018

Y2 - 26 April 2018 through 28 April 2018

ER -

ID: 13668908