کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
1715389 1519978 2012 6 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Suborbital and low-thermospheric experiments using sounding rockets in Taiwan
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
پیش نمایش صفحه اول مقاله
Suborbital and low-thermospheric experiments using sounding rockets in Taiwan
چکیده انگلیسی

The suborbital flight is a kind of flight, which reaches the space and then comes back to ground without completing one orbital revolution. The atmospheric thermosphere extends from 85 km to 600 km in altitude. Therefore, the suborbital and low-thermospheric experiments to be performed at altitude below 300 km can be combined using the sounding rocket. These experiments include rocket staging, fairing separation, ultrasonic flight, reentry, aerobrake and recovery test, ultraviolet and ionization observations, ozone measurement, etc. The advent of Taiwan's sub-orbital and thermospheric experiments project can be traced back to 1997. This is the year Taiwan's National Space Organization (NSPO) was assigned to be responsible for procuring the sounding rocket for applications in science experiments and space technology research effort. From 1997 to 2010, 8 launches have been completed including one experimental hybrid rocket. All onboard instruments and sensors for sub-orbital and low-thermospheric experiments are developed and integrated by the domestic universities. More launches have been planned in the future. Opportunities for international cooperation in developing new instruments and payloads for future experiments will be possible.


► Advent of Taiwan's sub-orbital and thermospheric experiments using sounding rockets has been described in detail.
► From 1997 to 2010, 8 launches have been completed including one experimental hybrid rocket.
► It is intended to transfer the sub-orbital and thermospheric experiments to domestic universities in the future.
► Opportunities for international cooperation in developing new instruments and payloads for future experiments would be possible.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Acta Astronautica - Volume 70, January–February 2012, Pages 159–164
نویسندگان
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