Sub‐Melt Consolidation of Aerospace‐Grade Thermoplastic Composites for High‐Rate Processing

J Joseph G. Kirchhoff (Walker Department of Mechanical Engineering University of Texas at Austin Austin TX 78712 USA) S Saeed Khaleghi (Department of Structural Engineering University of California San Diego La Jolla CA 92093 USA) G Greg Haugstad (Characterization Facility University of Minnesota Minneapolis MN 55455 USA) T Tyler B. Hudson (Advanced Materials and Processing Branch NASA Langley Research Center Hampton VA 23681 USA) M Mehran Tehrani (Program in Materials Science and Engineering University of California San Diego La Jolla CA 92093 USA)

Abstract

Abstract The processing of thermoplastic composites is often limited by high energy demands and slow cycle times. Out‐of‐autoclave amorphous/crystalline thermoplastic materials for energy‐efficient aerospace‐grade laminates (OATMEAL) addresses these challenges through a unique prepreg architecture. OATMEAL consists of slow‐cooled carbon fiber‐reinforced semicrystalline polyetheretherketone (PEEK) tape sheathed in thin amorphous polyetherimide (PEI) layers. The PEI sheaths are miscible with PEEK and enable interfacial healing below the melting point of PEEK—preserving pre‐existing crystallinity and reducing processing temperatures by 80 °C. The sheaths are thinned via high‐frequency laser ablation down to the PEEK–PEI blending regions, thereby reducing residual stresses and promoting chemical resistance. Fast‐cooled vacuum‐bag‐only oven processing of OATMEAL laminates yields aerospace‐quality parts while enabling processing speeds more than five times faster and reducing energy use by roughly 75% compared with conventional methods. These results represent a significant advancement and a step toward truly high‐rate, large‐scale aerostructure manufacturing.

Article Details

Volume / Issue Vol. 38, Issue 9
Published February 01, 2026
ISSN 0935-9648
Publisher Unknown Publisher

Journal Info

Advanced Materials

Unknown Publisher

ISSN: 0935-9648 Physical Sciences

Authors (5)

J

Joseph G. Kirchhoff

Walker Department of Mechanical Engineering University of Texas at Austin Austin TX 78712 USA

S

Saeed Khaleghi

Department of Structural Engineering University of California San Diego La Jolla CA 92093 USA

G

Greg Haugstad

Characterization Facility University of Minnesota Minneapolis MN 55455 USA

T

Tyler B. Hudson

Advanced Materials and Processing Branch NASA Langley Research Center Hampton VA 23681 USA

M

Mehran Tehrani

Program in Materials Science and Engineering University of California San Diego La Jolla CA 92093 USA