Influence of Thermal Treatment on Preceramic Polymer Grafted Nanoparticle Network Formation: Implications for Thermal Protection Systems and Aerospace Propulsion Components

Kara L. Martin, Caitlyn M. Clarkson, Christina Thompson, Gary Germanton, Nicholas Posey, Lutz Wiegart, Subramanian Ramakrishnan, Matthew B. Dickerson

Research output: Contribution to journalArticlepeer-review

4 Scopus citations

Abstract

Preceramic polymer grafted nanoparticles (PCP GNPs) offer potential advantages in the production of polymer-derived ceramic composites compared to neat preceramic polymers (PCPs), such as reduced thermal shrinkage and increased char yield. In comparison to traditional composites (particles + free polymer), PCPs avoid issues of compatibility, agglomeration, and phase separation during processing and provide routes to control nanoparticle arrangement. Prior literature has established that the conversion efficiency of PCPs and PCP GNPs to ceramics and ceramic composites is linked to the thermal pretreatment of these precursor polymers (e.g., curing). Herein, we investigate the material transformations that occur when exposing PCP GNPs to a low-temperature thermal treatment (≤250 °C) prior to pyrolysis. The PCP GNPs explored in this study possessed silica nanoparticle cores but were distinct in their PCP coronas, having poly(1,1-dimethylpropylsilane) (allyl-GNP)- or poly(1,1-dimethylbenzylethylsilane) (styryl-GNP)-grafted polymers. After undergoing low-temperature thermal treatment, these PCP GNPs exhibited increased char yield at 800 °C; however, unlike commercial PCPs (e.g., allylhydridopolycarbosilane (SMP-10)), obvious cross-linkable sites are not present in the PCP corona structure. Differential scanning calorimetry, oscillatory rheology, and X-ray photon correlation spectroscopy were utilized to elucidate the thermally induced material changes in the allyl- and styryl-GNPs. Thermally induced changes to the structure and behavior of the PCP GNPs were determined to be linked to the chemical structure of the grafted polycarbosilane chains. Styryl-GNPs experienced a curing event between 180 and 250 °C, effecting the formation of a network, which contributed to char yield improvement (at 800 °C). The nanoscale dynamics of this material also shows a transition from diffuse behavior to ballistic behavior because of the cross-linking event. Conversely, the allyl-GNPs did not exhibit a curing event under heat treatment but did show an increase in thermally induced physical cross-linking. The allyl-GNP physical network is stronger after the first cycle of thermal treatment, and it is considered that this contributed to the improvement in char yield post thermal treatment. The advancements in the understanding of the cross-linking behavior of these hybrid materials are expected to advance the application of these materials to turbine engine, advanced friction, and heat-shielding components.

Original languageEnglish
Pages (from-to)15288-15297
Number of pages10
JournalACS Applied Nano Materials
Volume5
Issue number10
DOIs
StatePublished - Oct 28 2022
Externally publishedYes

Funding

The authors declare no competing financial interests. The authors gratefully acknowledge funding from the Air Force Research Laboratory and Air Force Office of Scientific Research (AFOSR). We would like to thank Dr. Ming-Jen Pan, the program officer for the Aerospace Composites Portfolios, for his support of our research. Research was performed by UES employees (KLM) on site at AFRL/RX under contract FA8650-21-D-5279. This research was undertaken while CMC held an NRC Research Associateship award at the Air Force Research Laboratory. S. Ramakrishnan would like to acknowledge partial funding from the NSF FAMU CREST center award # 1735968 and the Department of Defense proposal number 76182-MS-REP, agreement number W911NF-20-1-0263. This research used resources and the Coherent Hard X-ray Scattering (CHX, 11-ID) beamline of the National Synchrotron Light Source II, a U.S. Department of Energy (DOE) Office of Science User Facility operated for the DOE Office of Science by Brookhaven National Laboratory under contract no. DE-SC0012704. Distribution A: Approved for public release: distribution unlimited. AFRL-2022-4675.

FundersFunder number
NSF FAMU1735968
U.S. Department of DefenseW911NF-20-1-0263, 76182-MS-REP
U.S. Department of Energy
Air Force Office of Scientific Research
Office of Science
Brookhaven National LaboratoryDE-SC0012704
Air Force Research Laboratory

    Keywords

    • X-ray photon correlation spectroscopy
    • char yield
    • polymer derived ceramics
    • polymer-grafted nanoparticles
    • preceramic polymers
    • rheology
    • thermal analysis

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