Thermal Control Subsystems
Thermal Control Subsystems is a technological framework within spacecraft engineering that regulates temperature distribution across components through active and passive elements to maintain operational conditions within predefined limits.
218
Publications
6.7K
Citations
623
Authors
184
Institutions
Publications per year
2017–2026
28
Parents
218
1–5 of 218
623
7
h-index
5
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5
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4
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h-index
1–5 of 623
184
Johnson Space Center
Houston, United States
11 h-index
19 publications
334 citations

Ames Research Center
Mountain View, United States
10 h-index
23 publications
750 citations

Langley Research Center
Hampton, United States
9 h-index
14 publications
298 citations
Jet Propulsion Laboratory
Pasadena, United States
9 h-index
30 publications
914 citations
Goddard Space Flight Center
Greenbelt, United States
8 h-index
13 publications
534 citations
Lockheed Martin (United States)
Bethesda, United States
8 h-index
14 publications
329 citations

European Space Research and Technology Centre
Noordwijk-Binnen, The Netherlands
7 h-index
10 publications
224 citations
Purdue University West Lafayette
West Lafayette, United States
6 h-index
11 publications
462 citations
1–8 of 184
72 publications · 2.1K citations
25
h-index
19 publications · 375 citations
14
h-index
11 publications · 664 citations
10
h-index
7 publications · 129 citations
7
h-index
6 publications · 240 citations
6
h-index
1–5