摘要
In the near-Earth satellites and spacecraft are continually subjected to extremes of temperature, flow of direct sunlight and temperatures close to absolute zero the interstellar medium. Heat balance models consider the radiative flux in the approach of equilibrium condition little relisted in MEO and GEO satellites. We use a non-equilibrium approximation to show that the true thermal evolution. Additionally we discuss the potential application of this model for Venesat-1 satellite.
| 源语言 | 英语 |
|---|---|
| 页 | 83-86 |
| 页数 | 4 |
| 出版状态 | 已出版 - 2010 |
| 活动 | 1st Russia and Pacific Conference on Computer Technology and Applications, RPC 2010 - Vladivostok, 俄罗斯联邦 期限: 6 9月 2010 → 9 9月 2010 |
会议
| 会议 | 1st Russia and Pacific Conference on Computer Technology and Applications, RPC 2010 |
|---|---|
| 国家/地区 | 俄罗斯联邦 |
| 市 | Vladivostok |
| 时期 | 6/09/10 → 9/09/10 |
学术指纹
探究 'Analytical time-dependent model for satellite thermal balance' 的科研主题。它们共同构成独一无二的学术指纹。引用此
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