Chinese Space Science and Technology
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Xu Jiwan Jiang Jingshan Qian Shengyu Zhang Shiling (Beijing Institute of Spacecraft Systems Engineering)
Online:
Abstract: This paper presents the thermal design and thermal testingof the chinese balloon satellite.According to the characteristics of theballoon satellite,the method of passive thermal control used in thermaldesign is described.The temperatures derived from the thermal testingdata are in agreement with those from the thermal calculating data.Thetemperatures of the balloon satellites have met the design requirements.
Xu Jiwan Jiang Jingshan Qian Shengyu Zhang Shiling (Beijing Institute of Spacecraft Systems Engineering). THERMAL DESIGN FOR DQ-1 BALLOON SATELLITE[J]. Chinese Space Science and Technology.
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URL: https://journal26.magtechjournal.com/kjkxjs/EN/
https://journal26.magtechjournal.com/kjkxjs/EN/Y1993/V13/I02/
