2022
DOI: 10.1016/j.jaap.2021.105397
|View full text |Cite
|
Sign up to set email alerts
|

Study of the degradation of epoxy resins used in spacecraft components by thermogravimetry and fast pyrolysis

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1

Citation Types

0
4
0

Year Published

2022
2022
2024
2024

Publication Types

Select...
7

Relationship

0
7

Authors

Journals

citations
Cited by 22 publications
(4 citation statements)
references
References 25 publications
0
4
0
Order By: Relevance
“…As a result, large quantities of permanent gas, such as CO and CH 4 , would be released during pyrolysis. 18 The elemental and proximate analysis of epoxy plastics (EP) measured in the laboratory was shown in Table 1. The migration of N and S elements was a significant method for studying the mechanism of gasification, and many researchers have investigated the migration of N and S elements.…”
Section: Methodsmentioning
confidence: 99%
See 1 more Smart Citation
“…As a result, large quantities of permanent gas, such as CO and CH 4 , would be released during pyrolysis. 18 The elemental and proximate analysis of epoxy plastics (EP) measured in the laboratory was shown in Table 1. The migration of N and S elements was a significant method for studying the mechanism of gasification, and many researchers have investigated the migration of N and S elements.…”
Section: Methodsmentioning
confidence: 99%
“…It was shown that there were eight degrees of unsaturation (double benzene ring) in the monomer. As a result, large quantities of permanent gas, such as CO and CH 4 , would be released during pyrolysis …”
Section: Methodsmentioning
confidence: 99%
“…21,31,52,53 Neat epoxy resin has the first weight loss (10.4%) from 270 to 320 C (Figure 8c), which is mainly attributed to decomposition of epoxy functional groups and the thermal desorption of organic molecules such as aliphatic ether. The compounds released over 320 C are mostly bisphenol, [58][59][60][61][62] which represents 47.9% of mass loss (Figure 8b). TGA indicates that capsules exhibit excellent thermal stability, exceeding 180 C. 51 Table 3 shows the TGA of species releases or degraded in function of temperature and mass loss (%).…”
Section: Core Content and Thermal Stabilitymentioning
confidence: 99%
“…16,17 The volume shrinkage and thermal degradation of aged resin epoxy can lead to a decrease in compression properties. 18,19 Interfacial debonding between the fibers and resin matrix due to local thermal tends to occur between two intersecting yarns in aged composites. 20 The combined effects of resin degradation and interface cracks affect the mechanical behaviors of aged 3DAWCs, including quasi-static 21 and low-velocity impact properties.…”
mentioning
confidence: 99%