I. Introduction
As humans advance in deep space exploration, extraterrestrial spacecraft must develop the capability to perceive damage in their structures to evaluate subsequent mission performance. This is known as the in situ damage monitoring capability [1], [2]. To increase payload, spacecrafts widely use lightweight and high-strength carbon fiber-reinforced composites (CFRCs) as their structural materials. However, in situ damage monitoring technology for CFRCs is still in the exploratory stage.