PRESSURIZATION SYSTEM EMPLOYING LIQUID PRESSURANT FOR EFFECTING PROPELLANT FLOW IN A LIQUID PROPELLANT ROCKET

• 1. 一种低温液体火箭推进剂管路控制系统及液体火箭发动机 [P] . 中国专利： CN111271193A . 2020-06-12
• 2. 加压流动炉系统的流动介质的输送方法和加压流动炉系统 [P] . 中国专利： CN103453530B . 2017.07.14
• 3. Pressurization system and method for effecting propellant flow in a liquid propellant rocket [P] . 美国专利： US3320742A . 1967-05-23

  机译： 用于在液体推进剂火箭中实现推进剂流动的增压系统和方法

• 4. Method of propellant stowage, arming and initiation of propellant flow for a liquid fuel propulsion system in a liquid fuel rocket motor [P] . 美国专利： US2954670A . 1960-10-04

  机译： 用于液体燃料火箭发动机中的液体燃料推进系统的推进剂积载，武装和启动推进剂流的方法

• 5. METHOD OF OPERATION OF LIQUID-PROPELLANT ROCKET ENGINE WITH TURBOPUMP DELIVERY OF CRYOGENIC PROPELLANT ON BASIS OF OXYGEN OXIDIZER AND HYDROCARBON FUEL AND LIQUID- PROPELLANT ROCKET ENGINE IMPLEMENTING SAID METHOD [P] . 俄罗斯专利： RU2197628C2 . 2003-01-27

  机译： 以氧气增氧剂和碳氢化合物为基础的加氢致冷剂涡轮泵输送液态推进剂火箭发动机的方法

• 1. First Systematic Testing Platform for Pressurization Feed System Developed for Liquid Rocket Propellant in China [J] . Zhang Yi 中国航天（英文版） . 2011,第003期
• 2. Effects of imidazolium-based ionic liquids on the isobaric vapor-liquid equilibria of methanol + dimethyl carbonate azeotropic systems [J] . Songsong Chen, Li Dong, Junping Zhang, 中国化学工程学报（英文版） . 2020,第003期
• 3. Characteristics of Droplets Ejected from Liquid Propellants Ablated by Laser Pulses in Laser Plasma Propulsion [J] . ZHENG Zhiyuan, GAO Hua, FAN Zhenjun, 等离子体科学和技术（英文版） . 2014,第003期
• 4. Modeling the effects of dissolved helium pressurant on a liquid hydrogen rocket propellant tank [C] . I A Richardson, J W Leachman Cryogenic Engineering Conference . 2018
• 5. Computer simulation of liquid and gaseous propellant run systems for rocket engine component ground test facilities. [D] . deQuay, Laurence. 1992
• 6. Examination of the liver in personnel working with liquid rocket propellant [O] . Palle Petersen, Erik Bredahl, Ove Lauritsen, 1970
• 7. Use of cryogenic components of propellants for liquid-propellant rocket engines and in life support systems of manned space vehicles [O] . Sergei A. Orlin 2020
• 8. Pressurization systems design guide. Volume 3 - Pressurant gas solubility in liquid propellants [R] . Cannon, W. A., English, W. D., Robson, J. H. 1968

• 1. On the Transient Numerical Simulation of Solid Rocket Motor by Coupling Quasi One⁃Dimension Internal Flow with Three⁃Dimension Propellant Grain Burnback [J] . Juan Duan ,Yongliang Xiong ,Ningdong Hu . 哈尔滨工业大学学报:英文版 . 2021,第5期
• 2. A Comparative Study of Genetic Algorithm Parameters for the Inverse Problem-based Fault Diagnosis of Liquid Rocket Propulsion Systems [J] . Erfu Yang ,Hongjun Xiang ,Dongbing Gu . 国际自动化与计算杂志：英文版 . 2007,第3期
• 3. 液体火箭发动机推进剂成分变化对燃烧性能影响研究 [C] . 查柏林 ,马云腾 ,徐志高 . 中国航空学会动力分会火箭发动机专业委员会2016年火箭推进技术学术年会 . 2016
• 4. 去氨加压素与硝普钠、艾司洛尔相比对功能性鼻内镜手术术野出血及血流动力学的影响 [A] . 杨寅奇 . 2019