Standard

Thermal deformation of 3U CubeSat in low Earth orbit. / Gorev, Vasily; Pelemeshko, Anatoly; Zadorozhny, Alexander et al.

In: MATEC Web of Conferences, Vol. 158, 01013, 19.03.2018.

Research output: Contribution to journal › Conference article › peer-review

Harvard

Gorev, V, Pelemeshko, A, Zadorozhny, A & Sidorchuk, A 2018, 'Thermal deformation of 3U CubeSat in low Earth orbit', MATEC Web of Conferences, vol. 158, 01013. https://doi.org/10.1051/matecconf/201815801013

APA

Gorev, V., Pelemeshko, A., Zadorozhny, A., & Sidorchuk, A. (2018). Thermal deformation of 3U CubeSat in low Earth orbit. MATEC Web of Conferences, 158, [01013]. https://doi.org/10.1051/matecconf/201815801013

Vancouver

Gorev V, Pelemeshko A, Zadorozhny A, Sidorchuk A. Thermal deformation of 3U CubeSat in low Earth orbit. MATEC Web of Conferences. 2018 Mar 19;158:01013. doi: 10.1051/matecconf/201815801013

Author

Gorev, Vasily ; Pelemeshko, Anatoly ; Zadorozhny, Alexander et al. / Thermal deformation of 3U CubeSat in low Earth orbit. In: MATEC Web of Conferences. 2018 ; Vol. 158.

BibTeX

@article{298e6a9c5680416db68bf18769b9d556,
title = "Thermal deformation of 3U CubeSat in low Earth orbit",
abstract = "The impact of uneven heating on a satellite structure in low Earth orbit has been considered using the example of 3U CubeSat. The calculations showed that the thermal deformation of CubeSat structure in orbit caused a deviation between normals to opposite small satellite sides of about 0.03°. Such a deviation is commensurate with the required satellite pointing accuracy approximately 0.1° necessary for satellite laser communication. It means that to solve similar problems in the CubeSat designing that require such or better CubeSat pointing accuracy, it is necessary to take into account the expected satellite structure thermal deformation.",
author = "Vasily Gorev and Anatoly Pelemeshko and Alexander Zadorozhny and Aleksey Sidorchuk",
year = "2018",
month = mar,
day = "19",
doi = "10.1051/matecconf/201815801013",
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 - Thermal deformation of 3U CubeSat in low Earth orbit

AU - Gorev, Vasily

AU - Pelemeshko, Anatoly

AU - Zadorozhny, Alexander

AU - Sidorchuk, Aleksey

PY - 2018/3/19

Y1 - 2018/3/19

N2 - The impact of uneven heating on a satellite structure in low Earth orbit has been considered using the example of 3U CubeSat. The calculations showed that the thermal deformation of CubeSat structure in orbit caused a deviation between normals to opposite small satellite sides of about 0.03°. Such a deviation is commensurate with the required satellite pointing accuracy approximately 0.1° necessary for satellite laser communication. It means that to solve similar problems in the CubeSat designing that require such or better CubeSat pointing accuracy, it is necessary to take into account the expected satellite structure thermal deformation.

AB - The impact of uneven heating on a satellite structure in low Earth orbit has been considered using the example of 3U CubeSat. The calculations showed that the thermal deformation of CubeSat structure in orbit caused a deviation between normals to opposite small satellite sides of about 0.03°. Such a deviation is commensurate with the required satellite pointing accuracy approximately 0.1° necessary for satellite laser communication. It means that to solve similar problems in the CubeSat designing that require such or better CubeSat pointing accuracy, it is necessary to take into account the expected satellite structure thermal deformation.

UR - http://www.scopus.com/inward/record.url?scp=85047721452&partnerID=8YFLogxK

U2 - 10.1051/matecconf/201815801013

DO - 10.1051/matecconf/201815801013

M3 - Conference article

AN - SCOPUS:85047721452

VL - 158

JO - MATEC Web of Conferences

JF - MATEC Web of Conferences

SN - 2261-236X

M1 - 01013

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

Y2 - 26 April 2018 through 28 April 2018

ER -

ID: 13668734