Courses - Spring 2026
ENAE696
Spacecraft Thermal Design
Credits:
3
Grad Meth:
Reg, Aud
Thermal sources in space. Black-body radiation; absorptivity and emissivity; radiative thermal equilibrium. Mutually radiating plates, view angles, and interior conduction. Techniques of spacecraft thermal analysis; approaches to passive and active thermal control.
Those sections that begin with a letter are designated for Master of Engineering students and are not intended for Master of Science or Ph.D.Students.
Flagship Institution of the University System of Maryland
University of Maryland, College Park, MD 20742, USA
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301.405.1000
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