TWO new ablative materials, designated SLA-741 and SLA-561, have been developed by Martin Marietta for Mars Lander thermal protection. The density range of these ablators is 0.18-0.22 g/cc and is substantially lower than that of other types of low density charring ablators. Plasma arc testing conducted in a simulated Mars atmosphere has established that SLA ablators are considerably more efficient than conventional ablators such as filled silicone, low density nylon-phenolic, or corkboard and that they form sturdy, erosion resistant chars.
New Ablative Heat Shield Materials for Mars Landers
Sae Technical Papers
National Aeronautic and Space Engineering and Manufacturing Meeting ; 1966
1966-02-01
Aufsatz (Konferenz)
Englisch
Delta II-launched Mars landers
AIAA | 1991
|Remote Recession Sensing of Ablative Heat Shield Materials
British Library Conference Proceedings | 2014
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