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Measuring Demisability of Bulk Metallic Glasses for Potential Satellite Applications through Ablation Experiments
Author(s) -
Bordeenithikasem Punnathat,
Roberts Scott N.,
Hofmann Douglas C.,
Ratliff John Martin,
Greene Benton R.,
Bacon John B.,
Sohn Sungwoo,
Schroers Jan
Publication year - 2020
Publication title -
advanced engineering materials
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.938
H-Index - 114
eISSN - 1527-2648
pISSN - 1438-1656
DOI - 10.1002/adem.202000708
Subject(s) - materials science , spacecraft , satellite , differential scanning calorimetry , amorphous metal , titanium , ablation , space debris , thermal , atmospheric entry , astrobiology , metallurgy , aerospace engineering , physics , thermodynamics , alloy , engineering
Bulk metallic glasses (BMGs) exhibit attractive properties for spacecraft applications. When low Earth‐orbiting satellites reenter the atmosphere at end of mission, a measure to mitigate the generation of space debris, operators must limit the number of satellite components that reach the ground to ensure public safety. Inductively coupled plasma using an argon/air mixture to simulate reentry conditions is used to study ablation of BMG and conventional spacecraft alloys. Differential scanning calorimetry is used to determine the thermal properties of the alloys. BMGs are shown to ablate similarly to aluminum alloys (Al7075) and dramatically faster than titanium alloys (Ti‐6Al‐4V).