FABRICATION AND PERFORMANCE OF LAUNCHING TUBE OF STAINLESS STEEL-COMPOSITE

Abstract

Abstract: Aiming at the defect of launching tube for rockets, a program has been proposed in which the stainless steel wasused as inner lining to prevent ablation of wake flame and the composite wasused as outer lining to guarantee strength and rigidity. And, thorough the research of sample performance, along with rockets launching, this program has been proved to meet the operating requirements sample parameters as follows: tensile strength 220MPa, tensile module 23.7GPa, compression intensity 153MPa, flexural strength 330MPa and layer trimming 24MPa.

Key words: stainless steel-composite, rockets, launching tube, light weight, repetitive use

CLC Number:

TB332

LUO Han. FABRICATION AND PERFORMANCE OF LAUNCHING TUBE OF STAINLESS STEEL-COMPOSITE[J]. COMPOSITES SCIENCE AND ENGINEERING, 2014, 0(4): 18-22.

References

[1] 付佺,李金龙,慕朝阳. 可以重复使用的便携式火箭发射器耐烧蚀涂层材料研究[J].弹箭与制导学报,2007,27(3):158-160.
[2] P M Radavich and A Selamet. A computational approach of America[J]. 2001,109(4):1022-1029.
[3] M J Ostrander, J L Bergmans, M E Thomas and S L Burroughs. Pintle motor challenges for tactical missiles[J]. AIAA,2000.
[4] 李涛,高兴,商伟辉等. 船舶用复合材料的性能研究[J].玻璃钢/复合材料,2011,217(2):32-35.
[5] 李明明,王晓洁,刘新东.树脂基复合材料耐海水性能研究进展[J].玻璃钢/复合材料,2011,217(2):60-64.
[6] 张中利,党玉功,乐贵高等. 玻璃钢定向器热弹性能数值仿真与分析[J].系统仿真学报,2010,22(4):877-880.
[7] 刘志明,韩珺礼,高敏. 火箭炮发射过程中火箭弹沿定向管运动分析[J].火炮发射与控制学报,2003,(2):7-11.
[8] 王轲,张福祥.玻璃钢制火箭炮定向器的强度研究[J].弹道学报,2003,15(2):39-48.
[9] 王兆飞,杨金柱,崔凯.基于箱式发射技术的定向器有限元分析[J].弹箭与制导学报,2012,32(1):222-224.
[10] 李玮, 段成红, 吴祥. 碳纤维复合材料强度的有限元模拟[J].玻璃钢/复合材料,2011,216(1):20-23.
[11] 徐亚栋,钱林方,陈龙淼.复合材料身管强迫响应分析复合材料身管强迫响应分析[J].玻璃钢/复合材料,2009,209(6):16-18.
[12] 王轩,李顶河,冯振宇等.复合材料层合板振动数值仿真[J].中国民航大学学报,2008,(01):23-26.
[13] 吴代华,晏石林,翟鹏程.层合板机械连接有限元分析[J].武汉理工大学学报, 1992,(02):18-21.
[14] 全国纤维增强塑料标准化技术委员会,中国标准出版社第五编辑室.纤维增强塑料(玻璃钢)标准汇编第二版[M].北京:中国标准出版社,2007.
[15] 总装备部电子信息基础部技术基础局等. GJB 150.1A-2009 军用装备实验室环境试验方法[S].北京:中国人民解放军总装备部,2009.