2008
DOI: 10.1061/(asce)0893-1321(2008)21:2(72)
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Technical Requirements for Lunar Structures

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Cited by 36 publications
(5 citation statements)
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“…It has been shown that the convection has negligible effects in hollow spheres with diameters less than 4 mm [10]. In addition, the flux due to radiation typically does not control heat transfer in composite foams [11]. As such, this study only considers conduction to model the flame retardant behavior of CMF.…”
Section: Flame Test Modelmentioning
confidence: 98%
“…It has been shown that the convection has negligible effects in hollow spheres with diameters less than 4 mm [10]. In addition, the flux due to radiation typically does not control heat transfer in composite foams [11]. As such, this study only considers conduction to model the flame retardant behavior of CMF.…”
Section: Flame Test Modelmentioning
confidence: 98%
“…The alternating day and night rhythm, which takes 14 days, results in extreme surface temperatures of –244 °C [23] at the poles and +122 °C in the equatorial zone as well as maximum temperature changes of up to 280 K [9]. These extreme conditions make high demands on materials and processing due to thermal expansion.…”
Section: Lunar Environmentmentioning
confidence: 99%
“…The internal pressure environment of the habitat set by NASA in conjunction with the lunar environment has specific design implications on the habitat (Jablonski, 2008). Due to the lack of atmosphere on the lunar surface and the internal pressure of the habitat, the predominant stress on the habitat while on the lunar surface is the internal pressure.…”
Section: Habitation Calculationsmentioning
confidence: 99%