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

Publisher: Edp Sciences

E-ISSN: 2261-236x|158|issue|01012-01012

ISSN: 2261-236x

Source: MATEC Web of conference, Vol.158, Iss.issue, 2018-03, pp. : 01012-01012

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Abstract