Spacecraft Power System Technologies by Qi Chen & Zhigang Liu & Xiaofeng Zhang & Liying Zhu

Author:Qi Chen & Zhigang Liu & Xiaofeng Zhang & Liying Zhu
Language: eng
Format: epub
ISBN: 9789811548390
Publisher: Springer Singapore

4.2 Design Example of Power System of the Satellite in Sun-Synchronous Orbit

Next, we take a satellite platform in sun-synchronous orbit designed in a generalized, serialized, and standardized way as an example to introduce its power system. This satellite operates in a sun-synchronous orbit, whose descending node is within the range of 10:00–14:00. It has a total mass of less than 3500 kg and a design lifetime of 8 years [3].

4.2.1 Design Conditions

In the power system design, the following constraints on power system have been considered:(1)Orbital characteristics and sunlight conditionsOrbit type: Sun-synchronous circular orbit, with the orbital period of 95 min;

Download

Copyright Disclaimer:
This site does not store any files on its server. We only index and link to content provided by other sites. Please contact the content providers to delete copyright contents if any and email us, we'll remove relevant links or contents immediately.