کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
1716413 | 1520000 | 2010 | 8 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Feasibility study of flight experiment for electrodynamic heatshield technology
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موضوعات مرتبط
مهندسی و علوم پایه
سایر رشته های مهندسی
مهندسی هوافضا
پیش نمایش صفحه اول مقاله
چکیده انگلیسی
The electrodynamic heatshield technique is a promising technique which can replace the current heatshield system. In addition, the technique can provide us a way to maneuver the vehicle without moving parts such as rudders. So far, much research has been devoted to this technique. Nevertheless the technology is remained to be verified by a flight experiment which is necessary since the existing ground facility cannot provide the flight condition. In this study, the feasibility of the flight experiment in a ballistic flight is critically discussed. Especially the super-conducting magnetic field generator and the measurement system onboard the vehicle are discussed in detail.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Acta Astronautica - Volume 66, Issues 5–6, March–April 2010, Pages 929–936
Journal: Acta Astronautica - Volume 66, Issues 5–6, March–April 2010, Pages 929–936
نویسندگان
Takashi Abe,