Method and tools for the manufacture of moulded parts, in particular of charge of solid propellant for rocket, and using these charges cartridges

• 1. 用于制造固体火箭发动机装药药柱的复合熔芯 [P] . 中国专利： CN210152806U . 2020.03.17
• 2. 用于固体火箭发动机装药的胀紧装置及施工方法 [P] . 中国专利： CN110630405B . 2021.06.18
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  机译： 固体火箭炮发动机中固体推进剂点火的方法和装置

• 4. Propellant charge of solid propellants for rocket, in particular for rocket lanceamarre [P] . 法国专利： FR1538180A . 1968-08-30

  机译： 固体火箭推进剂的推进剂，特别是用于火箭矛状体的推进剂

• 5. Arrangement for improving the burning efficiency of a rocket- borne solid propellant charge cartridge [P] . 美国专利： US4104969A . 1978-08-08

  机译： 改进火箭运载固体推进剂弹药筒燃烧效率的安排

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• 6. Application of charge density methods to a protein model compound: Calculation of Coulombic intermolecular interaction energies from the experimental charge density [O] . Xue Li, Guang Wu, Yuriy A. Abramov, 2002
• 7. Stress and strain state of the solid-propellant rocket engine charge fastened to the orthotropic body [O] . В.П. Печников 2013

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