The manner of utilization of rocket propellant

• 1. 一种污水回用处理及地热利用方式 [P] . 中国专利： CN112960824A . 2021-06-15
• 2. 基于土地利用方式优化的生态流量保障方法和装置 [P] . 中国专利： CN110738358A . 2020-01-31
• 3. The manner of utilization of rocket propellant [P] . PL380674A1 . 2008-03-31

  机译： 火箭推进剂的利用方式

• 4. Circulating head injector for combustion chamber that is utilized for rocket engine, has pipe having crown with channels whose ends emerge in groove, and propellant forming layer of propellant in groove before reaching another propellant [P] . 法国专利： FR2994713A1 . 2014-02-28

  机译： 用于火箭发动机的用于燃烧室的循环头喷射器，其管具有冠部，该冠部具有在端部出现在凹槽中的通道，并且在到达另一种推进剂之前在凹槽中形成推进剂层的推进剂

• 5. Higher-performance solid-rocket propellants and methods of utilizing them [P] . 美国专利： US8465607B1 . 2013-06-18

  机译： 高性能固体火箭推进剂及其利用方法

• 1. Ingredient and processing effects on the burning rates of composite rocket propellants utilizing a reduced-run mixture-process experiment design [J] . Frederick M. Gallant, Suzanne E. Prickett, Mario Cesarec, Chemometrics and Intelligent Laboratory Systems . 2008,第1期
• 2. Calculation of pressure in a solid-propellant rocket motor with the use of a real dependence of the solid propellant burning rate on pressure [J] . Lipanov A. M. Combustion, Explosion, and Shock Waves . 2017,第5期
• 3. Propellant Injector Influence on Liquid-Propellant Rocket Engine Instability [J] . Pavel P. Popov, William A. Sirignano, Athanasios Sideris Journal of propulsion and power . 2015,第1期
• 4. Development of a Liquid Propellant Rocket Utilizing Hydrogen Peroxide as a Monopropellant [C] . J. Lee, S. An, S. Kwon AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit . 2008
• 5. A simulation of the flow near a burning propellant in a solid propellant rocket motor. [D] . Ma, Yiping. 1990
• 6. Examination of the liver in personnel working with liquid rocket propellant [O] . Palle Petersen, Erik Bredahl, Ove Lauritsen, 1970
• 7. A proposal for the control of propellant utilization in a liquid bipropellant rocket engine [O] . Kastner Thomas M., McCullough Carlos D. 1957

• 1. A new experimental way for the monitoring of the real/equivalent inservice- time of double base rocket propellant by coupling VST and PCA [J] . Salim Chelouche ,Djalal Trache ,Ilyas Maamache . Defence Technology（防务技术） . 2021,第2期
• 2. 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
• 3. Composite Solid Rocket Propellant Based on GAP Polyurethane Matrix with Different Binder Contents [J] . Islam K .Boshra ,Ahmed Elbeih ,GUO Lin . 火炸药学报 . 2020,第004期
• 4. Overview of Physical and Chemical, Operational Properties of Nitrous Oxide Used as a Propellant for Low-thrust Rocket Engines [J] . A.A.Boryaev . 火炸药学报 . 2019,第1期
• 5. Studies on the Internal Ballistics of Composite Solid Rocket Propellants Incorporating Nano-Structured Catalysts [J] . Mukesh R. ,Sivasubramaniyam R. ,Elangovan R. R. . 航空科学与技术（英文） . 2017,第4期
• 6. 碳纳米管及其复合材料在固体火箭推进剂中的应用研究进展 [C] . PEI Jiang-feng ,裴江峰 ,ZHAO Feng-qi . 2013第十二届中国国际纳米科技（成都）研讨会 . 2013
• 7. 火箭推进剂加注装置优化设计与阻抗控制研究 [A] . 史剑峰 . 2015