“…However, typically, aircraft structures and components are not tested at these low temperatures where changes in the properties of materials may occur, particularly in composites where the difference in coefficient of thermal expansion between the matrix and fibres can result in the generation of thermal stresses, which might interact with impact damage created during maintenance, take-off and landing, causing microcracks to initiate and propagate at loads well below the ultimate strength of composite materials at low temperatures. 15,16 These issues have been largely ignored due to the difficulty in conducting reliable experiments, and instead, designs include large safety factors to account for uncertainty in structural performance at low temperature, which results in conservative and inefficient designs.…”