2013
DOI: 10.1115/1.4025367
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Thermal Insulators' Performances in Simulated Mars Environment

Abstract: This paper describes the experimental characterization of the thermal insulation properties of a multilayer insulator (MLI) and of an aerogel. Materials characterization wasperformed to optimize the thermal control design of a small interferometer devoted to planetary observation. In order to simulate the Martian environment, tests were performed in a carbon dioxide atmosphere, with pressures between 10 and 10'' Pa and temperatures from 193 to 353 K. MU was tested at different levels of layers compression to i… Show more

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Cited by 2 publications
(3 citation statements)
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“…1. The instrument comprises two heaters packaged respectively into an aluminium circular disk and on an external annulus [8]. The central disk provides an adjustable heat flux through the tested specimens.…”
Section: Setup Description and Testing Proceduresmentioning
confidence: 99%
See 1 more Smart Citation
“…1. The instrument comprises two heaters packaged respectively into an aluminium circular disk and on an external annulus [8]. The central disk provides an adjustable heat flux through the tested specimens.…”
Section: Setup Description and Testing Proceduresmentioning
confidence: 99%
“…number of layers, spacers material) [7,19], to the environment (interstitial gas pressure and temperature) [8], and therefore, cannot exempt from an experimental characterization.…”
Section: Introductionmentioning
confidence: 99%
“…At one standard atmosphere (1.0 atm, 101325 Pa), the thermal conductivity of SCQs (17.4 mW m −1 K −1 ) is much lower than that of MLIs (≈ 40 mW m −1 K −1 ) (Figure 6b). [ 29 ] Although in a thin atmosphere (0.0063 atm, 640 Pa), the thermal conductivity of SCQs (13.6 mW m −1 K −1 ) is less than half that of MLIs (≈30 mW m −1 K −1 ). Additionally, our SCQs also offer opportunities for thermal management in high humid environments or underwater conditions.…”
Section: Resultsmentioning
confidence: 99%