CAJ | 학술논문

研究了国产BHM3碳纤维原材料性能,制备了BHM3碳纤维/环氧648复合材料单向板结构,并将国产 BHM3 碳纤维应用到卫星结构件中.结果表明,国产 BHM3 碳纤维原材料拉伸强度为3100MPa,拉伸模量为400GPa;BHM3碳纤维/环氧648复合材料制备过程中工艺性良好,力学性能稳定;BHM3碳纤维卫星结构件的质量良好,均能够满足要求.
연구료국산BHM3탄섬유원재료성능,제비료BHM3탄섬유/배양648복합재료단향판결구,병장국산 BHM3 탄섬유응용도위성결구건중.결과표명,국산 BHM3 탄섬유원재료랍신강도위3100MPa,랍신모량위400GPa;BHM3탄섬유/배양648복합재료제비과정중공예성량호,역학성능은정;BHM3탄섬유위성결구건적질량량호,균능구만족요구.
Studied the performance of BHM3 carbon fiber, manufactured the unidirectional composites used BHM3 carbon fiber/epoxy 648, and applied the BHM3 carbon fiber in satellite structure. The results show that, the tensile strength of BHM3 carbon fiber is 3100MPa, and the tensile modulus is 400GPa. The manufacturability of BHM3 carbon fiber is well, and the mechanical properties are stability. The quality of the satellite structure is good, and can satisfy the requirements.