1997
DOI: 10.1080/00218469708014413
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Effect of Molecular Weight on Processing and Adhesive Properties of the Phenylethynyl-Terminated Polyimide LARC™-PETI-5

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Cited by 45 publications
(27 citation statements)
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“…26 As shown in Table 3, for example, as a result of the phenylethynyl group reaction, the T g of Oligo-1 had an obvious growth from 155 C to 326 C. All of the other oligomers displayed similar thermal behavior, and the T g s of the cured oligomers decrease correspondingly from 326 C to 280 C with the increasing of M n , which could be attributed to the cross-linking density. 19,36 All the films exhibited higher T g values than PETI-5 (270 C), 17 which indicated that these oligomers could be used at higher temperature.…”
Section: Thermal Properties Of the Oligomers And Thermally Cured Filmsmentioning
confidence: 97%
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“…26 As shown in Table 3, for example, as a result of the phenylethynyl group reaction, the T g of Oligo-1 had an obvious growth from 155 C to 326 C. All of the other oligomers displayed similar thermal behavior, and the T g s of the cured oligomers decrease correspondingly from 326 C to 280 C with the increasing of M n , which could be attributed to the cross-linking density. 19,36 All the films exhibited higher T g values than PETI-5 (270 C), 17 which indicated that these oligomers could be used at higher temperature.…”
Section: Thermal Properties Of the Oligomers And Thermally Cured Filmsmentioning
confidence: 97%
“…29,34,35 Furthermore, decreasing the molecular weights of the oligomers led to an apparent drop in the minimum melt viscosity, and at the same time, it provided a broader processing window as expected. 17,26,33 Isothermal viscosity measurements at 280 C were also conducted to test the melt stability. Figure 5 shows the melt viscosities of oligomers at 280 C for 1 h and Table 2 summaries the isothermal melt viscosity data of the aromatic …”
Section: Melt Processability Of Phenylethynly-terminated Oligomersmentioning
confidence: 99%
“…This material has a unique combination of properties including superior mechanical properties and thermal stability, excellent resistance to aircraft fluids, and easy processing in an au- toclave. To date, a composite system, PETI-5 reinforced with IM7 graphite fiber, has displayed promising performance, meeting the requirements of the HSCT program [2][3][4][5][6][7].…”
Section: Introductionmentioning
confidence: 99%
“…The extent of imidization can be determined from the heights of the absorption bands for imides I and III, terminated imide oligomers for high-temperature aerospace and aircraft applications, known as phenylethynyl-terminated imide (LaRC PETI), were developed at the National Aeronautics and Space Administration (NASA) Langley Research Center, USA [13][14][15][16][17][18][19]. These materials have broader processing windows and thermal oxidative stability than simple ethynyl-terminated materials, and consequently have many practical advantages as a potential material for coatings, adhesives, films, and composite matrix resins [20,21].…”
Section: Phenylethynyl-terminated Imide Polymermentioning
confidence: 99%