A method for ignite - of the inner and outer shell of a burner as a bending rockets formed fabric propellant fixedly set in combustion chambers and device for carrying out the method

• 1. 燃烧器组件、包括所述燃烧器组件的燃烧室以及将燃料供应到所述燃烧器组件的方法 [P] . 中国专利： CN105102894B . 2017.07.11
• 2. 燃烧器组件、包括所述燃烧器组件的燃烧室以及将燃料供应到所述燃烧器组件的方法 [P] . 中国专利： CN105102894A . 2015-11-25
• 3. Device for ignite of the inner and outer shell of a burner as a bending, which is firmly substance rocket propellant charge. [P] . 德国专利： DE000001751268C . 1972-03-30

  机译： 用于弯曲燃烧器的内壳和外壳的装置，该装置牢固地是火箭推进剂装药。

• 4. Device for ignite of the inner and outer shell of a burner as a bending, which is firmly substance rocket propellant charge. [P] . 德国专利： DE1751268B1 . 1971-08-12

  机译： 用于弯曲燃烧器的内壳和外壳的装置，该装置牢固地是火箭推进剂装药。

• 5. Device for ignite of the inner and outer shell of a burner designed as a bending tenfeststofftreibsatzes rocket propellant 12. [P] . 德国专利： DE1776192B2 . 1971-09-23

  机译： 燃烧器的内壳和外壳的点燃装置，设计成弯曲的tenfeststofftreibsatze火箭推进剂12。

• 1. Using Thermal Methods to Understand the Interactions between a Rocket Propellant and Igniter Material [C] . Ruth Tunnell International Confederation for Thermal Analysis and Calorimetry Congress 2016 . 2016
• 2. Comparison of standard test methods for measuring the performance of waterproof, windproof, and breathable shell fabrics. [D] . Kwon, Myoungsook. 2001
• 3. Innovative methodology for calculation and design of liquid-propellant rocket engine combustion chamber [O] . О.В. Короткая 2016
• 4. A Comparison of Experimental Heat Transfer Coefficients in a Nozzle with Analytical Predictions from Bartz's Methods for Various Combustion Chamber Pressures in a Solid Propellant Rocket Motor [R] . Smith, D. M. 1970

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