CAJ | 학술논문

以提高NEPE推进剂粘合剂体系力学性能为研究目的，从调整NEPE推进剂粘合剂基体交联网络结构的角度，提出了粘合剂配方设计思路，并运用凝胶点预测理论，推导出固化参数计算公式RT＝Pc fI-fI/fH；通过测试不同固化参数的胶片的力学性能，寻找到了凝胶点的经验值为0．80～0．90；同时，通过实例介绍了进行配方设计的步骤，验证了固化参数计算公式的正确性。
이제고NEPE추진제점합제체계역학성능위연구목적，종조정NEPE추진제점합제기체교련망락결구적각도，제출료점합제배방설계사로，병운용응효점예측이론，추도출고화삼수계산공식RT＝Pc fI-fI/fH；통과측시불동고화삼수적효편적역학성능，심조도료응효점적경험치위0．80～0．90；동시，통과실례개소료진행배방설계적보취，험증료고화삼수계산공식적정학성。
In order to improve the mechanical properties of NEPE propellant binder system,from the adjustment of crosslinking network structure of NEPE propellant binder matrix,the binder formulation design was proposed,and using the gel point prediction theory,the curing parameter calculation formula RT=PcfI-fI/fH was deduced.By testing the mechanical properties of adhesive with different curing parameters,the experience value of gel point is 0.80~0.90;meanwhile,through the specific example,the procedures of formulation design were introduced,validating the correctness of curing parameter calculation formula.