CONCEPTION OF “SILENT” MORTAR PROJECTILE. PART I – REVIEW OF EXISTING DESIGNS

2021 ◽  
Vol 156 (1) ◽  
pp. 39-49
Author(s):  
Marcin GUTOWSKI ◽  
Mariusz MAGIER
Keyword(s):  

Theoretical introduction into operational principles and designs of typical “silent” mortars and their ammunition is presented in the paper. The principle of operation and structure of “silent” mortar projectile are presented. In the following chapters a review of selected designs of “silent” mortar projec-tiles is included. After analysing the data the final calibre of the projectile and other key parameters to be deployed in own project were accepted. Following designing parameters were accepted in the summary: calibre 60 mm, mass of the projectile 1.8 kg, minimum muzzle velocity 125 m/s.

2012 ◽  
Vol 496 ◽  
pp. 99-103
Author(s):  
Zhi Tao Liu ◽  
Dan Dan Ji ◽  
Bin Xu ◽  
Hong Xia Jia ◽  
Xin Liao

In order to get better interior ballistic performance of deterred-coating propellant charge (DCPC), the simulated annealing algorithm optimization of DCPC carries out in this paper. The interior ballistic model of DCPC and its model of simulated annealing algorithm optimization are established based on the characteristics of deterred-coating propellant. Two key parameters of DCPC, the mass ratio of deterred-coating propellants to total propellants and the average perforation pressure of deterred-coating propellant,are optimized for the search of the maximum muzzle velocity under the restricting conditions of maximum chamber pressure and the maximum relative end point of combustion. The optimization results agree well with the standard charge parameters, which justifies the feasibility of the model.


2014 ◽  
Vol 701-702 ◽  
pp. 1218-1222
Author(s):  
Yu Feng Zheng ◽  
Han Hong Jiang ◽  
Jun Yong Lu

Controlling the output current characteristic of the pulsed power system is the important approach to optimize the parameters and to heighten the system efficiency in the Electromagnetic Launching System. For enhancing the system performance, distributed-current-feed style is introduced. A distributed current feeding-in model is established and the characteristic and performance is analyzed. Stimulation depicts:1)adopting the distributed feeding style results in more efficient than the central feeding style ;2)employing the new method of distributed-feed-timing-discharging goes a step further to heighten the muzzle velocity. The new model is meaningful to optimize the structure of the electromagnetic launching system, and is effective to the design of the launcher and current-feeding-in system.


2014 ◽  
Vol 26 (4) ◽  
pp. 45040
Author(s):  
徐伟东 Xu Weidong ◽  
陈允 Chen Yun ◽  
袁伟群 Yuan Weiqun ◽  
赵莹 Zhao Ying ◽  
王咸斌 Wang Xianbin ◽  
...  

2010 ◽  
Vol 77 (5) ◽  
Author(s):  
Wei Yu ◽  
Xiaobing Zhang

During a gun firing, the flow around a projectile will be developing and changing. In particular, the flow around the projectile is disturbed significantly when the projectile overtakes the muzzle flow. Furthermore, the projectile body pressure will also change substantially. Therefore, the shot ejection process has an important effect on the shot accuracy. The maximum projectile velocity is one of the most important design goals of the interior ballistic process and also is the initial condition for the exterior ballistic process. Most researchers take the muzzle velocity as the maximum projectile velocity; actually, after the projectile exits the muzzle, the projectile velocity will increase further due to the influence of the muzzle flow. Most investigations of the muzzle flow focused on the blowout of the high-pressure jet flow after the projectile exited the muzzle. The interior ballistic process was ignored or simply assumed in most investigations. Also, the mutual influence between the moving projectile and the muzzle flow was often neglected. Actually, a precursor shock flow near the muzzle is formed before the projectile exits. This precursor muzzle flow has an important influence on the trajectory of the projectile, especially, for the prevalent trend of gun systems including large caliber cannon and multiple launch gun systems. For these reasons, the interior ballistic process was coupled with the simulation of the flow near the muzzle. A hybrid structured-unstructured gridding method was used to simulate the process from the projectile engraving to the gas ejection phase, accounting for the moving projectile. The simulation results show that the projectile muzzle velocity was 893.99 m/s but the maximum velocity was 899.28 m/s. The projectile velocity increased rapidly to up to 0.8 ms after muzzle exit; thereafter, the projectile velocity increased slowly before reaching its maximum value. The maximum Mach number of the effluent gas increased to 6.83 and the breech pressure decreased to 21.5 MPa at 1.8 ms after the projectile exited the muzzle. The formation and development of the muzzle flow field was highly complex and transient. The analysis of the projectile velocity was conducted during the interior ballistic after-effect period. The predicted muzzle velocity and maximum barrel pressure are in good agreement with those measured in gun firings. Results of the numerical simulation and analysis are helpful to understand and master the aerodynamic process of gun system launching and provide significant guidance for research into shot accuracy and muzzle brake design.


2011 ◽  
Vol 39 (1) ◽  
pp. 133-137 ◽  
Author(s):  
Thorbjörn Siaenen ◽  
Markus G. Schneider ◽  
Markus J. Loffler

2019 ◽  
Vol 147 (3/2018) ◽  
pp. 47-62
Author(s):  
Marek Radomski

The paper presents a lumped parameter mathematical model considering the changes of thermodynamic properties for combustion products of a composite propelling charge, and of a burning cartridge casing or shell as well, when shot with classic guns. In addition a method was proposed for considering not coincidental instants of ignition for particular components of the charge and also for powder grains of each component, and the heat flow into the walls containing the space with combustion products. Some results of numerical computations are shown for 125 mm 2A46 tank gun firing a hard core projectile. Moreover an evaluation of accuracy of the results is given on the basis of experimental data. Maximum pressure and muzzle velocity were basic criteria at the verification of the model. Analysis of accuracy for solutions of model equations allows a conclusion that the proposed mathematical model may be useful at the designing process of ammunition and guns.


Sign in / Sign up

Export Citation Format

Share Document