1996
DOI: 10.1088/0954-0083/8/4/002
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Processing and Properties of IM7/LARC ™ -RP46 Polyimide Composites

Abstract: LARC™-RP46 resin system is a PMR type polyimide and is prepared by replacing methylenedianiline in the PMR-15 composition with 3,4′-oxydianiline. This resin system retains the same processing characteristics as PMR-15 but also offers enhanced fracture toughness. Rheological measurements were conducted on pre-imidized LARC™-RP46 moulding powder subjected to various ramp and hold temperature schemes. Adequate flow properties were found with theoretical (formulated) molecular weight 6 ≤1500 g mol−1. Critical tran… Show more

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Cited by 30 publications
(34 citation statements)
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“…On the basis of the TG/FTIR/MS and DSC information, for RP46/IM7 prepreg curing, the overall analysis seemed to suggest the following: (1) the release of methanol and water between 100 and 280°C with a peak at 138–140°C for both, indicating the loss of absorbed moisture and residual methanol as well as that from the formation of imidized prepolymer, and (2) the formation of cyclopentadiene between 200 and 400°C with a peak within 310–350°C. Thus, the prepolymerization and thermal crosslinking reaction sequence proposed by the National Aeronautics and Space Administration (NASA) LARC group11 was confirmed by this real‐time evolved‐gas analysis. They essentially followed the curing reaction paths of the AFR700B/T650‐35 prepreg.…”
Section: Resultssupporting
confidence: 67%
“…On the basis of the TG/FTIR/MS and DSC information, for RP46/IM7 prepreg curing, the overall analysis seemed to suggest the following: (1) the release of methanol and water between 100 and 280°C with a peak at 138–140°C for both, indicating the loss of absorbed moisture and residual methanol as well as that from the formation of imidized prepolymer, and (2) the formation of cyclopentadiene between 200 and 400°C with a peak within 310–350°C. Thus, the prepolymerization and thermal crosslinking reaction sequence proposed by the National Aeronautics and Space Administration (NASA) LARC group11 was confirmed by this real‐time evolved‐gas analysis. They essentially followed the curing reaction paths of the AFR700B/T650‐35 prepreg.…”
Section: Resultssupporting
confidence: 67%
“…11 Pater and co-workers studied lower toxicity PMR formulations based on 3,4 0 -oxydianiline. 12,13 However, many of these early replacements had lower T g s and thermal oxidative stability than PMR-15. To address these issues, researchers studied and patented the utilization of mixtures of non-toxic, exible, multi-ring bisanilines in combination with single ring bisanilines.…”
Section: Introductionmentioning
confidence: 99%
“… The chemical structures of the matrix materials investigated in this work. The reaction scheme for LaRC‐RP46 was adapted from ref 6…”
Section: Resultsmentioning
confidence: 99%
“…Most material names are registered trademarks, which are not additionally denoted in the text. Three thermoset materials were selected based on their high temperature performance: Matrimide 5292 (Vantico), a two‐component bismaleimide (BMI) resin consisting of 4,4′‐bismaleimidodiphenyl methane (A) and 3,3″‐diallyl bisphenol‐A (B); AroCy XU371 (Vantico), an experimental novolac cyanate ester, catalyzed by 2 wt.‐% of a mixture of 3 wt.‐% Co(acac) 3 in nonylphenol (Arcos Chemicals); and LaRC‐RP46,6–8 a B‐staged molding powder, based on polyimide and bisnadimide chemistry. Subsequently AroCy XU371 has been discontinued, but Lonza sells a similar resin as Primaset PT30.…”
Section: Experimental Partmentioning
confidence: 99%