航天推进技术研究院主办
Chen Zhijian,Li Zhi,Wu Jianjun.Research on propellant tank composite diaphragm[J].Journal of Rocket Propulsion,2005,31(01):21-23.
推进剂贮箱复合膜研究
- Title:
- Research on propellant tank composite diaphragm
- 分类号:
- V258
- 文献标志码:
- A
- 摘要:
- 系统分析了液体推进剂对隔膜式贮箱中隔膜材料的腐蚀和渗透规律,提出了采用镀膜技术进行金属和非金属材料复合的方案来解决推进剂的渗透问题。初步试验结果证明,复合膜技术在降低材料渗透率方面有着明显的优势。
相似文献/References:
[1]姚娜,顾仁年,鲍国苗,等.适用于负过载启动的新型增压输送系统[J].火箭推进,2007,33(02):12.
Yao Na,Gu Rennian,Bao Guomiao.New pressurization and propellant feed system for aircraft start-up under negative G condition[J].Journal of Rocket Propulsion,2007,33(01):12.
[2]梁小强.凝胶试验系统的设计及试后处理工艺[J].火箭推进,2006,32(04):51.
Liang Xiaoqiang.Design of test system for gel propellants and processing measures after tests[J].Journal of Rocket Propulsion,2006,32(01):51.
[3]李龙飞.MESSENGER飞船推进剂贮箱的设计与制造[J].火箭推进,2004,(02):41.
[4]张轩,王旭阳,徐自力,等.冲击载荷下姿轨控贮箱流固耦合响应分析[J].火箭推进,2024,50(03):19.[doi:10.3969/j.issn.1672-9374.2024.03.003]
ZHANG Xuan,WANG Xuyang,XU Zili,et al.Fluid-solid coupling response analysis of propellant tank in attitude-orbit control system under impact load[J].Journal of Rocket Propulsion,2024,50(01):19.[doi:10.3969/j.issn.1672-9374.2024.03.003]