کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
1716165 | 1520004 | 2009 | 15 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
A series of small scientific satellite with flexible standard bus
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کلمات کلیدی
موضوعات مرتبط
مهندسی و علوم پایه
سایر رشته های مهندسی
مهندسی هوافضا
پیش نمایش صفحه اول مقاله
![عکس صفحه اول مقاله: A series of small scientific satellite with flexible standard bus A series of small scientific satellite with flexible standard bus](/preview/png/1716165.png)
چکیده انگلیسی
Japan Aerospace Exploration Agency has a plan to develop the small satellite standard bus for various scientific missions and disaster monitoring missions. The satellite bus is a class of 250–400 kg mass with three-axis control capability of 0.02∘0.02∘ accuracy. The science missions include X-ray astronomy missions, planetary telescope missions, and magnetosphere atmosphere missions. In order to adapt the wide range of mission requirements, the satellite bus has to be provided with flexibility. The concepts of modularization, reusability, and product line are applied to the standard bus system. This paper describes the characteristics of the small satellite standard bus which will be firstly launched in 2011.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Acta Astronautica - Volume 65, Issues 9–10, November–December 2009, Pages 1345–1359
Journal: Acta Astronautica - Volume 65, Issues 9–10, November–December 2009, Pages 1345–1359
نویسندگان
Hirobumi Saito, Syujiro Sawai, Shin-ichiro Sakai, Seisuke Fukuda, Kenji Kitade,