2018
DOI: 10.5028/jatm.v10.1011
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Thermal Analysis of Satellite Libertad 2: a Guide to CubeSat Temperature Prediction

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Cited by 24 publications
(2 citation statements)
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“…For sake of ease, these properties can be averaged over the full effective area of the spacecraft, following the guidelines from [7] and [8] in this way:…”
Section: Table 2 Spacecraft External Optical Propertiesmentioning
confidence: 99%
“…For sake of ease, these properties can be averaged over the full effective area of the spacecraft, following the guidelines from [7] and [8] in this way:…”
Section: Table 2 Spacecraft External Optical Propertiesmentioning
confidence: 99%
“…The potential effects of this temperature change on satellite subsystems must be predicted and analyzed in different development phases such as design, simulation, test, and verification [2][3][4]. This issue is more crucial for spacecrafts since they must survive the thermal tensions caused by the motion in the dense part of the atmosphere during the ascent and the reentry phases of the mission, and the thermal effects due to direct radiations.…”
Section: Introductionmentioning
confidence: 99%