Studies on RDX Rarticle Size in LOVA Gun Propellant Formulations

A. G. S. Pillai; R. R. Sanghavi; DC. R. Dayanandan; M. M. Joshi; S. P. Velapure; Amarjit Singh

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Studies on RDX Rarticle Size in LOVA Gun Propellant Formulations

机译：LOVA炮药配方中RDX弹丸尺寸的研究。

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This paper presents the results of systematic studies carried out on the role of fine RDX in determining the burning rate and ballistics of LOVA gun propellants. Propellant formulations containing fine RDX particles with a size of 4.5, 6, 13 and 32 #mu#m as energetic ingredient, cellulose acetate as inert binder, triacetin as inert plasticizer, nitrocelluose of lower percentage nitrogen content as energetic binder and carbamite as stabilizer were made. The evalution of the propellant batches has been carried out by static firing using closed vessel technique. It indicates the lienar relation between the burning rate of the propellant and the fine RDX particle size used in this formulation. The results of the present studies revealed that fine RDX of 4.5 to 6 #mu#m size may be the most sutiable for LOVA gun propellant to meet the desired burning rate for satisfactory ballistics.

机译：本文介绍了对RDX细粉在确定LOVA火药推进剂燃烧速率和弹道方面的作用进行的系统研究的结果。含有4.5、6、13和32＃mu＃m大小的RDX细颗粒作为能量成分，乙酸纤维素作为惰性粘合剂，三醋精作为惰性增塑剂，氮含量较低的硝化纤维素作为能量粘合剂以及氨基甲酸酯作为稳定剂的推进剂配方为制作。使用封闭容器技术通过静态燃烧对推进剂批次进行了评估。它表明了该配方中推进剂的燃烧速率与RDX细粒度之间的关连关系。本研究的结果表明，尺寸为4.5至6＃μm的精细RDX可能是LOVA炮推进剂满足要求的燃烧速度以获得令人满意的弹道的最合适方法。

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《Propellants, Explosives, Pyrotechnics》 |2001年第5期|共3页
作者
A. G. S. Pillai; R. R. Sanghavi; DC. R. Dayanandan; M. M. Joshi; S. P. Velapure; Amarjit Singh;
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正文语种 eng
中图分类爆炸物工业、火柴工业;
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1. Studies on RDX Rarticle Size in LOVA Gun Propellant Formulations [J] . A. G. S. Pillai, R. R. Sanghavi, DC. R. Dayanandan, Propellants, Explosives, Pyrotechnics . 2001,第5期

机译：LOVA炮药配方中RDX弹丸尺寸的研究。
2. Role of Bimodal RDX in LOVA Gun Propellant Combustion [J] . A.G.S. Pillai, B. R. Gandhe, C. R. Dayanandan, Defence science journal . 2013,第3期

机译：双峰RDX在LOVA火药推进剂燃烧中的作用
3. Studies on the Effects of RDX Particle Size on the Burning Rate of Gun Propellants [J] . A.G.S. Pillai, C. R. Dayanandan, M. M. Joshi, Defence science journal . 2013,第2期

机译：RDX粒度对枪推进剂燃烧速率影响的研究
4. Processibility and Combustion Properties of LOVA Propellant with the Size of RDX Particle [C] . Soon Kil Kwon, Jeong Hwan Lee, Jun Sik Hwang, International Autumn Seminar on Propellants, Explosives and Pyrotechnics(2003 IASPEP); 20031015-18; Guilin(CN) . 2003

机译：具有RDX颗粒尺寸的LOVA推进剂的可加工性和燃烧性能
5. Multidimensional modeling of solid propellant burning rates and aluminum agglomeration and one-dimensional modeling of RDX/GAP and AP/HTPB. [D] . Tanner, Matthew W. 2008

机译：固体推进剂燃烧速率和铝团块的多维建模以及RDX / GAP和AP / HTPB的一维建模。
6. Experimental Study of Pyrolysis and Laser Ignition of Low-Vulnerability Propellants Based on RDX [O] . Jordan Ehrhardt, Léo Courty, Philippe Gillard, 2020

机译：基于RDX的低脆弱性推进剂热解和激光点火实验研究
7. Study on Mechanical Properties of Gun-propellants with RDX.doc [O] . Liu Jiaa, Cheng Shan, Wang Yan-hong, 2016

机译：RDX.doc对枪推进剂力学性能的研究
8. Combustion Product Evaluation of Various Charge Sizes and Propellant Formulations. Task 1 Report: Sampling and Analytical Procedures Proposed for Use in Gun Propellant Combustion Product Characterization. [R] . Taylor, K., Gordon, S., Ase, P., 1988

机译：各种电荷尺寸和推进剂配方的燃烧产物评估。任务1报告：建议用于喷枪推进剂燃烧产物表征的采样和分析程序。

Studies on RDX Rarticle Size in LOVA Gun Propellant Formulations

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