Henry C A. Thermoplastic composites rocket propellant: USP4361526[P]. 1982.
[2]
Paik Sung C S,Smith T W. Properties of segmented polyether PUU based on 2,4-TDI[J]. Macromolecules,1980(13): 117-121.
[3]
何吉宇,谭惠民. 推进剂用热塑性聚酯聚氨酯弹性体的结构与性能[J]. 宇航学报,2005,26(1): 86-89.HE Ji-yu,TAN Hui-min. Morphology and properties of thermoplastic polyester polyurethane elastomer for propellants[J]. Journal of Astonautics,2005,26(1): 86-89.
[4]
张素珍. 环氧乙烷四氢呋喃共聚醚的结构与性能[J]. 北京理工大学学报，1992,12(S1): 39-47.ZHANG Su-zhen. Morphology and properties of tetrahydrofuran-ethylene oxide copolyether[J]. Beijing Institute of Technology,1992,12(S1): 39-47.
[5]
Ernie D B. Process for preparing solid propellant grains using thermoplastic binders and product thereof: USP4764316[P]. 1986.
[6]
Schollenberger C S,Hewitt L E. Differential scanning calorimetry analysis of morphological changes in segmented elastomers[J]. PolymPreprints,1978,19: 17-18.
[7]
Ernie D B. Process for preparing solid propellant grains using thermoplastic binders and product thereof: USP4764316[P]. 1986.
[8]
Ho Hyung Lee,Shank Won K. Structure and thermal propeties PUU elastomers[J]. Journal of Applied polymer Science,1993,50: 80-92.
[9]
Gerald E M. Thermoplatic elastomers having alternate orystalline structure for as high energy binder: USP5210153[P]. 1993.
[10]
菅晓霞,肖乐勤,左海丽,等. GAP基热塑性弹性体的合成及表征[J]. 含能材料,2008,16(4): 614-617.JIAN Xiao-xia，XIAO Le-qin,ZUO Hai-li,et al. Synthesis and characterization of GAP-based thermoplastic elastomer[J]. Chinese Journal of Energetic Materials(Hanneng Cailiao),2008,16(4): 614-617.
[11]
陈福泰,多英全,李晓萌,等. IPDI基热塑性聚醚聚氨酯弹性体的形态结构与性能[J]. 北京理工大学学报,2001,21(2): 260-265.CHEN Fu-tai,DUO Ying-quan,LI Xiao-meng,et al. Morphology and properties of thermoplastic polyether polyurethane based on IPDI[J]. Beijing Institute of Technology,2001,21(2): 260-265.
