کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
1718476 | 1013845 | 2012 | 10 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Numerical study on the thermal design of on-board blackbody
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موضوعات مرتبط
مهندسی و علوم پایه
سایر رشته های مهندسی
مهندسی هوافضا
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چکیده انگلیسی
On-board blackbody is used for radiation temperature calibration of spaceborne IR radiometers and imaging systems. The thermal design of blackbody proposed in this study consists of heaters to heat-up the blackbody during the calibration, heat pipe to transfer residual heat on the blackbody just after calibration to radiator on the spacecraft and heaters on the radiator to keep the certain temperature range of the blackbody during non-calibration. The effectiveness of thermal design of on-board blackbody has been investigated by on-orbit thermal analysis. Two types of blackbody with different heat pipe installation have also been proposed and numerically investigated to verify which design is more applicable for on-board blackbody.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Aerospace Science and Technology - Volume 18, Issue 1, April–May 2012, Pages 25–34
Journal: Aerospace Science and Technology - Volume 18, Issue 1, April–May 2012, Pages 25–34
نویسندگان
Hyun-Ung Oh, Somin Shin,