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simulations; (ii) diagnose and attribute the physical mechanisms driving inter-model differences in recovery; and (iii) design and run targeted mechanism-denial experiments (e.g., in CESM and related Earth
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emissions and environmental impact. This project will develop a high-enthalpy inductively coupled plasma torch system to simulate the extreme thermal environments of spacecraft atmospheric re-entry, enabling
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. Please include a copy of your CV and a cover letter, detailing how your skills and experience match the requirements of the role, in your application.
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