词条 | Silicone impregnated refractory ceramic ablator |
释义 |
SIRCA was used for ceramic substrates on both the Viking spacecraft and the Space Shuttle,[2] and was also used on the aeroshells for Mars Pathfinder and the Mars Exploration Rovers.[1] It was developed at NASA Ames Research Center in the 1980s and 1990s.[2] DescriptionSIRCA typically has a density between {{convert|0.20|-|0.40|g/cc|lb/ft3}} and can handle a heat flux of up to {{convert|300|W/cm2}}[1] and is easily machined to custom shapes.[2] References1. ^1 2 {{cite web |url=https://uknowledge.uky.edu/cgi/viewcontent.cgi?referer=https://duckduckgo.com/&httpsredir=1&article=1029&context=ablation |title=A Perspective on the Design and Development of the SpaceX Dragon Spacecraft Heatshield |last=Rasky|first=Daniel J. |publisher=NASA |date=2012-02-28 |accessdate=2018-03-19 }} {{engineering-stub}}2. ^1 2 {{cite conference |last=Sepka|first=Steven A. |last2=Samareh|first2=Jamshid A. |title=Thermal Protection System Mass Estimating Relationships for Blunt-Body, Earth Entry Spacecraft |url=https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20150018864.pdf |conference=45th AIAA Thermophysics Conference, Dallas Texas |date=26 June 2015 }} 1 : Spaceflight technologies |
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