東華大學圖書館 |

Language: English

Help

回圖書館首頁

手機版館藏查詢

Back

Switch To: Labeled | MARC Mode | ISBD

Predictive thermal analysis of the c...

Moffitt, Blake Almy.

Linked to FindBook

Google Book

Amazon

博客來

Predictive thermal analysis of the combat sentinel satellite test article.

Record Type:	Electronic resources : Monograph/item
Title/Author:	Predictive thermal analysis of the combat sentinel satellite test article./
Author:	Moffitt, Blake Almy.
Description:	182 p.
Notes:	Source: Masters Abstracts International, Volume: 41-06, page: 1764.
Contained By:	Masters Abstracts International41-06.
Subject:	Engineering, Aerospace. -
Online resource:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1413839

Predictive thermal analysis of the combat sentinel satellite test article.
Moffitt, Blake Almy.

Predictive thermal analysis of the combat sentinel satellite test article. - 182 p.

Source: Masters Abstracts International, Volume: 41-06, page: 1764.

Thesis (M.S.)--Utah State University, 2003.

A detailed study of a small satellite thermal response to irradiation has been performed. This study analyzed the response of the Combat Sentinel Satellite Test Article (CSSTA) to an external radiation environment.Subjects--Topical Terms:

1018395
Engineering, Aerospace.

Predictive thermal analysis of the combat sentinel satellite test article.
LDR:01717nmm 2200265 4500 001 1810212
005 20040126131523.5
008 130610s2003 eng d
035 $a (UnM)AAI1413839
035 $a AAI1413839
040 $a UnM $c UnM
100 1 $a Moffitt, Blake Almy. $3 1671038
245 1 0 $a Predictive thermal analysis of the combat sentinel satellite test article.
300 $a 182 p.
500 $a Source: Masters Abstracts International, Volume: 41-06, page: 1764.
500 $a Major Professor: J. Clair Batty.
502 $a Thesis (M.S.)--Utah State University, 2003.
520 $a A detailed study of a small satellite thermal response to irradiation has been performed. This study analyzed the response of the Combat Sentinel Satellite Test Article (CSSTA) to an external radiation environment.
520 $a Once the irradiation thermal response of the satellite materials was understood, two thermal models of the satellite test article were created. The first thermal model was a 13-element lumped capacitance model. This model was used to study the thermal response of CSSTA as a function of heat transfer parameters. The 13-element model also provided a baseline solution to compare the final more detailed thermal model of the satellite. Following the creation of the 13-element model, a detailed I-deas Thermal Model Generator (TMG) model of the satellite was created. This model began as several individual TMG models of satellite components. (Abstract shortened by UMI.)
590 $a School code: 0241.
650 4 $a Engineering, Aerospace. $3 1018395
690 $a 0538
710 2 0 $a Utah State University. $3 960049
773 0 $t Masters Abstracts International $g 41-06.
790 1 0 $a Batty, J. Clair, $e advisor
790 $a 0241
791 $a M.S.
792 $a 2003
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1413839