Carbon Fiber Oxidation in 4D

B Benjamin M. Ringel (Department of Aerospace Engineering, Grainger College of Engineering University of Illinois at Urbana‐Champaign 104 S Wright Street Urbana IL 61802 USA) F Federico Semeraro J Joseph C. Ferguson (Analytical Mechanics Associates NASA Ames Research Center Moffett Field CA 94035 USA) H Harold S. Barnard (Advanced Light Source Lawrence Berkeley National Laboratory Berkeley CA 94720 USA) B Bruno Dias (Analytical Mechanics Associates NASA Ames Research Center Moffett Field CA 94035 USA) C Christian M. Schlepütz (Swiss Light Source Paul Scherrer Institute Forschungsstrasse 111 5232 Villigen Switzerland) E Edward S. Barnard (Molecular Foundry Lawrence Berkeley National Laboratory Berkeley CA 94720 USA) S Sam Schickler (Advanced Light Source Lawrence Berkeley National Laboratory Berkeley CA 94720 USA) K Kara Levy (Advanced Light Source Lawrence Berkeley National Laboratory Berkeley CA 94720 USA) S Shawn Shacterman (Advanced Light Source Lawrence Berkeley National Laboratory Berkeley CA 94720 USA) T Talia Benioff‐White (Advanced Light Source Lawrence Berkeley National Laboratory Berkeley CA 94720 USA) J Julian Davis (Department of Engineering, University of Southern Indiana) A Alastair A. MacDowell (Advanced Light Source Lawrence Berkeley National Laboratory Berkeley CA 94720 USA) D Dilworth Y. Parkinson F Francesco Panerai (Department of Aerospace Engineering, Grainger College of Engineering University of Illinois at Urbana‐Champaign 104 S Wright Street Urbana IL 61802 USA)

Abstract

Abstract The oxidation of carbon fibers at high temperatures is the primary degradation process in the thermal protection system of many hypersonic flight vehicles. Predicting the rate and the extent of oxidation is critical to ensure a safe and effective design. An oversized thermal protection system adds unnecessary mass, while an under‐designed one risks system failure and mission loss. Resolving high‐temperature material degradation due to oxidation has been a long‐standing challenge in designing for re‐entry flight environments. Using time‐resolved in situ X‐ray microtomography, the oxidation of carbon fibers at high temperatures is directly imaged, resolving the two limiting degradation regimes: diffusion‐ and reaction‐limited. The ability to resolve material degradation in time at the sub‐micron scale sheds light on the ablation phenomenon and enables predictions of material constitutive properties evolving in time, with profound implications on the ability to model the aerothermal response of heat shield materials in hostile environments.

Article Details

Volume / Issue Vol. 37, Issue 42
Published October 01, 2025
ISSN 0935-9648
Publisher Unknown Publisher

Journal Info

Advanced Materials

Unknown Publisher

ISSN: 0935-9648 Physical Sciences

Authors (15)

B

Benjamin M. Ringel

Department of Aerospace Engineering, Grainger College of Engineering University of Illinois at Urbana‐Champaign 104 S Wright Street Urbana IL 61802 USA

F

Federico Semeraro

J

Joseph C. Ferguson

Analytical Mechanics Associates NASA Ames Research Center Moffett Field CA 94035 USA

H

Harold S. Barnard

Advanced Light Source Lawrence Berkeley National Laboratory Berkeley CA 94720 USA

B

Bruno Dias

Analytical Mechanics Associates NASA Ames Research Center Moffett Field CA 94035 USA

C

Christian M. Schlepütz

Swiss Light Source Paul Scherrer Institute Forschungsstrasse 111 5232 Villigen Switzerland

E

Edward S. Barnard

Molecular Foundry Lawrence Berkeley National Laboratory Berkeley CA 94720 USA

S

Sam Schickler

Advanced Light Source Lawrence Berkeley National Laboratory Berkeley CA 94720 USA

K

Kara Levy

Advanced Light Source Lawrence Berkeley National Laboratory Berkeley CA 94720 USA

S

Shawn Shacterman

Advanced Light Source Lawrence Berkeley National Laboratory Berkeley CA 94720 USA

T

Talia Benioff‐White

Advanced Light Source Lawrence Berkeley National Laboratory Berkeley CA 94720 USA

J

Julian Davis

Department of Engineering, University of Southern Indiana

A

Alastair A. MacDowell

Advanced Light Source Lawrence Berkeley National Laboratory Berkeley CA 94720 USA

D

Dilworth Y. Parkinson

F

Francesco Panerai

Department of Aerospace Engineering, Grainger College of Engineering University of Illinois at Urbana‐Champaign 104 S Wright Street Urbana IL 61802 USA