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Thermal Control for a 1000 km Orbit ...

Vadehra, Arujun Singh.

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Thermal Control for a 1000 km Orbit Microsatellite.

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Thermal Control for a 1000 km Orbit Microsatellite./
作者:	Vadehra, Arujun Singh.
出版者:	Ann Arbor : ProQuest Dissertations & Theses, : 2023,
面頁冊數:	106 p.
附註:	Source: Masters Abstracts International, Volume: 85-05.
Contained By:	Masters Abstracts International85-05.
標題:	Aerospace engineering. -
電子資源:	https://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=30640310
ISBN:	9798380842730

Thermal Control for a 1000 km Orbit Microsatellite.
Vadehra, Arujun Singh.

Thermal Control for a 1000 km Orbit Microsatellite. - Ann Arbor : ProQuest Dissertations & Theses, 2023 - 106 p.

Source: Masters Abstracts International, Volume: 85-05.

Thesis (M.A.S.)--University of Toronto (Canada), 2023.

The Space Flight Laboratory, with its focus on the micro-space philosophy, strives to make space more accessible. This thesis describes the thermal design for a DEFIANT microsatellite, a prime example of the laboratory's modular spacecraft platforms. To be operated at an altitude of 1000 kilometers, this spacecraft pushes the limits of what the DEFIANT platform has achieved. The many stages of spacecraft thermal model development and testing are described. Reference thermal designs are presented that prove the viability of thermal control for the mission. This higher altitude mission also requires an active de-orbiting strategy. The impact this additional phase has on spacecraft lifetime thermal behavior is investigated. The challenges of multi-altitude thermal design are highlighted. Finalized thermal control for launch is detailed using findings from de-orbiting investigations. The unique aspects of this mission demonstrate the Laboratory's ability to innovate and redefine what can be achieved with small spacecraft.

ISBN: 9798380842730Subjects--Topical Terms:

1002622
Aerospace engineering.
Subjects--Index Terms:

Deorbit

Thermal Control for a 1000 km Orbit Microsatellite.
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245 1 0 $a Thermal Control for a 1000 km Orbit Microsatellite.
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300 $a 106 p.
500 $a Source: Masters Abstracts International, Volume: 85-05.
500 $a Advisor: Zee, Robert E.
502 $a Thesis (M.A.S.)--University of Toronto (Canada), 2023.
520 $a The Space Flight Laboratory, with its focus on the micro-space philosophy, strives to make space more accessible. This thesis describes the thermal design for a DEFIANT microsatellite, a prime example of the laboratory's modular spacecraft platforms. To be operated at an altitude of 1000 kilometers, this spacecraft pushes the limits of what the DEFIANT platform has achieved. The many stages of spacecraft thermal model development and testing are described. Reference thermal designs are presented that prove the viability of thermal control for the mission. This higher altitude mission also requires an active de-orbiting strategy. The impact this additional phase has on spacecraft lifetime thermal behavior is investigated. The challenges of multi-altitude thermal design are highlighted. Finalized thermal control for launch is detailed using findings from de-orbiting investigations. The unique aspects of this mission demonstrate the Laboratory's ability to innovate and redefine what can be achieved with small spacecraft.
590 $a School code: 0779.
650 4 $a Aerospace engineering. $3 1002622
650 4 $a Mechanical engineering. $3 649730
650 4 $a Physics. $3 516296
650 4 $a Condensed matter physics. $3 3173567
653 $a Deorbit
653 $a Orbits
653 $a Satellites
653 $a Spacecrafts
653 $a Testing
653 $a Thermal behavior
690 $a 0538
690 $a 0548
690 $a 0611
690 $a 0605
710 2 $a University of Toronto (Canada). $b Aerospace Science and Engineering. $3 2105951
773 0 $t Masters Abstracts International $g 85-05.
790 $a 0779
791 $a M.A.S.
792 $a 2023
793 $a English
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