Arbeider med HTCE

Date Issued
2006
Keywords
Herding
Raketter - Brensel
Project number
2006/02841
Permalink
http://hdl.handle.net/20.500.12242/1948
Collection
Rapporter
06-02841.pdf
Size: 3M
Abstract
Various polymer matrices intended for future application in rocket propellants were prepared and characterized. All samples were based on the prepolymer hydroxyl terminated poly-caprolactone ether (HTCE) which was cured with Desmodur N100. Two types of curing catalysts were used: DBTDL and TFB. The plasticizer BDNPA/F was mixed into one of the polymer matrices. The curing reaction was analyzed by FTIR and rheology analysis, whereas cured samples were subjected to hardness measurements (Shore A) and themoanalysis (DSC and TGA).
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