Polyimides are attractive for high temperature applications as the matrix r
esins, due to their excellent thermo-oxidative stability and mechanical pro
perties. As composite materials for aerospace applications, they possess ce
rtain unique characteristics such as toughness, resistance to temperature a
nd solvents as well as high tensile strength and modulus. A series of novel
PMR polyimides based on substituted benzidines are examined and compared t
o the state-of-the-art PMR-15. The assigned glass transition temperatures a
nd the mechanism for the thermal decomposition of four specific PMR polyimi
des are obtained, using thermal mechanical analysis and TGA/FTIR/MS techniq
ues, Their thermal decomposition steps are proposed, identified and also co
mpared to each other. (C) 2001 Elsevier Science B.V. All rights reserved.