The present invention relates to a
solid rocket engine
propellant lining layer material and a preparation method thereof, and belongs to the field of
solid rocket engine lining layer material preparation. According to the present invention, azido-terminated
polybutadiene is adopted as a
polymer prepolymer, a multi-alkynyl compound is adopted as a curing agent, a
plasticizer, a
solid filler and a process auxiliary agent are added, and an inter-azido / alkynyl
click chemistry reaction is used to prepare the
triazole five-membered ring cross-linked low-polarity
polybutadiene lining layer material, such that the migration performance of the polar
nitrate plasticizer of the NEPE composite
propellant in the lining layer material is effectively inhibited; and the obtained solid
rocket engine
propellant lining layer material can be subjected to curing molding within the temperature of 50-70 DEG C, the
reaction conditions are mild, the obtained lining layer material has low polarity, the disadvantages of the propellant lining layer material preparation through the cross-linking of
polyurethane and
polybutadiene are overcome, and the propellant lining layer material preparation method is broadened.