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Characteristic Property of Combustion and Internal Ballistics of Triple-Based Propellant including RDX 含RDX的三基推进剂燃烧特性及内弹道
Pub Date : 2022-06-05 DOI: 10.9766/kimst.2022.25.3.321
Soojung Son, Wonmin Lee, William David Lee, Soon-Kil Kwon, Jinyoung Jung
The current development tend of the gun propellants that they should have low sensitivity and high energy. We studied a nitrocellulose based propellant composition that replaced sensitive NG with RDX and DEGDN which high energy and low sensitivity. The important factors in the design of the gun propellant were impetus and flame temperature. NC-based propellant containing RDX showed similar impetus but low flame temperature compared to KM30A1, a triple-based propellant. The developed propellant composition didn’t show any abnormal combustion reaction and the characteristics of ballistic resistance were also confirmed.
低灵敏度高能量是当前火炮推进剂的发展趋势。研究了一种以高能量、低灵敏度的RDX和DEGDN代替敏感NG的硝化纤维素基推进剂组合物。推力和火焰温度是火炮发射药设计的重要因素。含有RDX的nc基推进剂与三基推进剂KM30A1相比,具有相似的推力,但火焰温度较低。研制的推进剂成分未发生异常燃烧反应,弹道阻力特性也得到了证实。
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引用次数: 1
The Study of Optimal Performance Improvement Method for Aircraft of Various Variants within the Same Type 同型多变型飞机性能优化改进方法研究
Pub Date : 2022-06-05 DOI: 10.9766/kimst.2022.25.3.311
Youngil Kim, Seung-Mo Ahn, Myeongseok Choi
In this paper, we studied the optimal method of improving performance for aircraft having various variants within the same type. The study defined configuration of an entire fleet of aircraft being subject to a performance improvement program. And selected the most complicated aircraft configuration among them as a Standard Aircraft for modification by according to the proposed Aircraft Selection Process for developing an optimal Aircraft Performance Improvement Process. Based on the selected the Standard Aircraft, drew a system integration design result and carried out Evaluation Test and obtained Airworthiness Certification. Created the database with the design data of the Standard Aircraft, Evaluation Test, and Airworthiness Certification results, and applied it to variants of aircraft to complete the performance improvement program with optimized schedules and costs. By applying the proposed method to IFF performance improvement program, drew optimal system integration design and completed the program with minimized schedule.
本文研究了在同一型号具有多种型号飞机的情况下,提高飞机性能的最佳方法。该研究定义了整个机队的配置,并将其纳入性能改进计划。并根据提出的飞机选择流程,选择其中构型最复杂的飞机作为标准飞机进行改装,从而制定出最优的飞机性能改进流程。在选定标准飞机的基础上,得出了系统集成设计结果,并进行了评估试验,获得了适航审定。根据标准飞机的设计数据、评估测试和适航认证结果创建数据库,并将其应用于飞机的各种型号,以优化时间表和成本完成性能改进计划。将该方法应用于敌我识别系统的性能改进方案,绘制出最优的系统集成设计方案,并以最小的进度完成方案。
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引用次数: 0
The Study on the Performance Prediction of Precision Linear Shaped Charge Using Numerical Analysis Method 基于数值分析方法的精密线性聚能药性能预测研究
Pub Date : 2022-06-05 DOI: 10.9766/kimst.2022.25.3.275
S. Lee
Linear Shaped Charge(LSC) is widely used as a separation system in the field of weapon system. However, there are some disadvantages that are charging lots of explosives due to lack of uniformity and having difficulties of the design of liner and explosives because of manufacturing process. In order to solve these problems, Precision Linear Shaped Charge(PLSC) that can design a liner independently and charge explosives uniformly has been developed. In this study, PLSC was designed to have a proper liner shape and amount of explosives, and the penetration test of PLSC with different stand-off distance from liner to target was conducted. On the basis of the penetration test results of PLSC, the numerical analysis method using AUTODYN was established and verified. The penetrative mechanism and characteristics of PLSC with targets of different materials was analyzed from experimental and numerical results.
线聚能作为一种分离系统在武器系统领域得到了广泛的应用。但其缺点是由于装药不均匀导致装药量大,以及由于制造工艺的原因给衬里和炸药的设计带来困难。为了解决这些问题,研制出了一种能够独立设计药管并能均匀装药的精密直线聚能药。在本研究中,设计了合适的衬垫形状和炸药量的PLSC,并进行了不同衬垫与目标距离的PLSC侵彻试验。在PLSC侵透试验结果的基础上,建立并验证了基于AUTODYN的数值分析方法。从实验和数值结果两方面分析了PLSC对不同材料靶材的侵彻机理和特性。
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引用次数: 0
A Study of Test and Evaluation Method for Performance Improvement of Air to Ground Communication Radios 空对地通信无线电性能改进测试与评价方法研究
Pub Date : 2022-06-05 DOI: 10.9766/kimst.2022.25.3.267
Byeongheon Lee, S. Ahn, Myungsuk Choi, Jang-wook Hur
The Republic of Korea has a close cooperative relationship with NATO, of which the United States is a member. NATO is encouraged to follow UHF coalition waveforms for military air operations(SATURN) as defined in STANAG 4372. SATURN is a high-speed frequency hopping waveform with enhanced anti-jamming and security functions. Plans to improve the performance of existing military aircraft with air to ground radios to which SATURN function is applied. IFF case analysis and MRT evaluation plan were established to present an efficient test and evaluation plan for air to ground radios.
大韩民国与美国是北约成员的北约有着密切的合作关系。鼓励北约采用STANAG 4372中规定的用于军事空中行动的超高频联合波形(SATURN)。SATURN是一种高速跳频波形,具有增强的抗干扰和安全功能。计划通过应用土星功能的空对地无线电来改善现有军用飞机的性能。建立敌我识别案例分析和MRT评估方案,为空对地无线电提供高效的测试评估方案。
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引用次数: 0
Analysis on Infrared Stealth Performance of Metal Nano-coating on Radome Surface 天线罩表面金属纳米涂层红外隐身性能分析
Pub Date : 2022-06-05 DOI: 10.9766/kimst.2022.25.3.251
Yongwoo Lee, Injoong Chang, Juyeong Nam, H. Bae, H. Cho
Infrared stealth technology used in aircraft is applied to reduce the infrared signal by controlling surface temperature and emissivity using internal heat sink, low emissivity material or metamaterial. However, there is one part of the aircraft where the use of this technology is limited, and that is the radome. Especially, radome should have transmittance for the specific radio frequency, therefore, common stealth technology such as emissivity control surfaces cannot be applied to radome surface. In this study, we developed metal nano-coating for infrared stealth which is applicable to radome surface. We designed slot-type pattern for frequency selective transmission in X-band, and also controlled thickness of metal nano-coating for long wavelength infrared emissivity control. As a result, our infrared stealth surface for radome has 93.2 % transmittance in X-band and various infrared emissivities from 0.17 to 0.57 according to nano-coatings thickness. Also, we analyzed infrared signature of radome through numerical simulation, and finally reduced contrast radiant intensity by 97.57 % compared to polyurethane surface.
飞机红外隐身技术是利用内部散热片、低发射率材料或超材料,通过控制飞机表面温度和发射率来降低红外信号的技术。然而,在飞机的一个部分,这种技术的使用是有限的,那就是天线罩。特别是天线罩对于特定的射频要有透射率,因此发射率控制面等常见的隐身技术不能应用于天线罩表面。在本研究中,我们开发了一种适用于雷达罩表面的红外隐身金属纳米涂层。我们设计了狭缝型模式,用于x波段的频率选择传输,并控制金属纳米涂层的厚度,用于控制长波红外发射率。结果表明,雷达罩红外隐身表面的x波段透过率为93.2%,红外发射率随纳米涂层厚度的变化范围为0.17 ~ 0.57。通过数值模拟分析了雷达罩的红外特征,与聚氨酯表面相比,雷达罩的对比辐射强度降低了97.57%。
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引用次数: 0
A Research on Intercommunication Method for Tactical Information Among Heterogeneous Mobile Combat Vehicles 异构机动作战车辆间战术信息互通方法研究
Pub Date : 2022-04-05 DOI: 10.9766/kimst.2022.25.2.187
Il-Ho Choi, Hae-Whan No, Choong-Ho Song
Modern Battle Fields are covered with various weapon systems, such as tanks, infantry vehicles, or artillery vehilces. In such environment, it is important to take it into consideration what kind of efficient method should be developed to communicate with heterogeneous friend combat systems for the exchange of tactical information aqcuired because military operations require coordinated actions. For this purpose, we made a research on tactical information equipments such as Battlefield Management Systems(BMSs) equipped in multiple kinds of Mobile Combat Vehicles(MCVs). The exchange of tactical information could be divieded into separate domains, such as connectivity, messages, and recognition processes by operators. In this article, we will deal with wireless radio connectivity, KVMF messages, and User Interfaces showing shared data.
现代战场上覆盖着各种武器系统,如坦克、步兵车辆或火炮车辆。在这样的环境下,由于军事行动需要协同行动,必须考虑采用何种有效的方法与异构友方作战系统进行通信,以交换所获得的战术信息。为此,对多种机动战车装备的战场管理系统(bms)等战术信息设备进行了研究。战术信息的交换可以被划分到不同的领域,如连接、消息和操作员的识别过程。在本文中,我们将处理无线无线电连接、KVMF消息和显示共享数据的用户界面。
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引用次数: 0
Direction Finding and Tracking using Single-Ring Circular Array Antenna and Space Division Table 基于单环圆阵列天线和空间分割表的测向与跟踪
Pub Date : 2022-04-05 DOI: 10.9766/kimst.2022.25.2.117
Hyeon Park, D. Woo, Jaesik Kim, Jinsung Park
Single-ring circular array antennas can be applied to direction finding systems in order to use nose-section in other purposes, and the interferometry is a proper direction finding method to those systems. We usually make the interferometer baseline long enough to achieve good angular accuracy. However, an interferometer with baseline longer than a half-wavelength has the ambiguity problem. In this paper, we present a novel method for solving the ambiguity problem in interferometry systems. This technique is based on the amplitude comparison method and the space division table, and it can place a target within the angular region in which the ambiguity problem does not occur by roughly estimating direction-of-arrival. The Monte Carlo simulation results show that proposed method can effectively remove the ambiguity problem in the system.
单环圆阵天线可以应用于测向系统中,以实现机头部分的其他用途,干涉测量法是测向系统的一种合适的测向方法。我们通常使干涉仪基线足够长,以达到良好的角度精度。但是,基线长度大于半波长的干涉仪存在模糊问题。本文提出了一种解决干涉测量系统中模糊问题的新方法。该方法基于幅度比较法和空间分割表,通过对到达方向的粗略估计,将目标定位在不存在模糊问题的角度区域内。蒙特卡罗仿真结果表明,该方法能有效地消除系统中的模糊问题。
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引用次数: 0
Mark XIIA(Mode 5) IFF System Integration and Certification Test for Surface to Air Missile System Mark XIIA(模式5)地空导弹系统敌我识别系统集成与认证试验
Pub Date : 2022-04-05 DOI: 10.9766/kimst.2022.25.2.160
Woo-Hyun Kim, Se-Young Jung, Yun-Soo Lee, Se-Myong Chang
The new IFF mode, Mode-5 replacing Mode-4, has already been established by the US DoD for its allies and NATO forces. A IFF retrofit program for replacing the Mark XII Mode-4 with Mark XIIA Mode-5 is in progress in order to overcome the security limitations of the former in R.O.K. IFF certification test for the new mode, Mode-5, has been performed on medium range surface to air missile platform of the Korean armed forces for the first time in R.O.K and this is regarded as a monumental event in Korean defense industry. The present paper is a discussion on the procedures applied to the IFF system retrofit and integration, lessons learned from AIMS test with the US AIMS PO as observer. The minimum modification from the existing Mark XII Mode-4 to Mark XIIA Mode-5 and evolutional adaption from previous design including interoperability are required for the system retrofit. Letter of Certification was received from the US AIMS PO after the tests. The authors propose that the lessons learned and know-how acquired during the tests are managed by the R.O.K Government as the standard structure of a database. It is expected that the use of the database will reduce the developmental difficulties and risk, also increase efficiency in future developments and other projects.
美国国防部已经为其盟国和北约部队建立了新的敌我识别模式,即模式-5取代模式-4。目前,韩国正在推进用“Mark XIIA -5”代替“Mark XIIA -4”的敌我识别(IFF)改装计划。该计划是为了克服“Mark XIIA -5”在韩国国内的安全性限制,首次在韩国军队的中程地空导弹平台上进行敌我识别(IFF)验证试验,这被认为是韩国国防工业的重大事件。本文讨论了敌我识别系统改造和集成的程序,以及美国AIMS PO作为观察员进行的AIMS试验的经验教训。从现有的Mark XII Mode-4到Mark XIIA Mode-5的最小修改以及从以前的设计(包括互操作性)的进化适应是系统改造所必需的。测试结束后收到美国AIMS PO的认证信。提交人建议,在测试期间获得的经验教训和专门知识由韩国政府作为数据库的标准结构加以管理。预期数据库的使用将减少发展的困难和风险,并提高今后发展和其他项目的效率。
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引用次数: 3
Research on Applicability of Laser Ablation Propulsion to Space Debris Removal by Simulations 激光烧蚀推进在空间碎片清除中的适用性仿真研究
Pub Date : 2022-04-05 DOI: 10.9766/kimst.2022.25.2.169
S. Yoo, Seung-Min Lee
Laser ablation propulsion(LAP) is the method to create impulse by laser ablation. It can be used to deorbit the space debris(SD), as its long-range property and versatility on any material. In this paper, we find out several requirements of the LAP system(LAPS) to deorbit the SD by simple numerical calculations of the SD orbit and laser beam flux. As a result, minimum operable altitude angle turned out to be a crucial variable to the LAPS. Moreover, if minimum operable altitude angle is 10°, and if the minimum distance between the LAPS and the SD is below 450 km, 1 m/s2 is sufficient to deorbit the SD by once. With 18 kJ/3 ns pulsed laser and cube shaped 100 kg SD, 1 m/s2 acceleration can be achieved by increasing the pulse repetition rate over 34~53 Hz, depending on the size of the SD. This capability could compare with the conceptual design of the Japan Establishment for a Power-laser Community Harvest(J-EPoCH) facility, which include 8 kJ, 5 PW@100 Hz laser.
激光烧蚀推进(LAP)是一种利用激光烧蚀产生脉冲的方法。由于其远程特性和在任何材料上的通用性,它可用于空间碎片脱轨。本文通过对SD轨道和激光束通量的简单数值计算,得出了LAP系统(LAPS)对SD脱轨的几个要求。因此,最小可操作高度角是影响LAPS的关键变量。此外,如果最小可操作高度角为10°,并且lap与SD之间的最小距离低于450 km,则1m /s2足以使SD脱轨一次。在18 kJ/3 ns的脉冲激光和100 kg的立方体SD下,根据SD的大小,在34~53 Hz范围内增加脉冲重复频率可以实现1 m/s2的加速度。这种能力可以与日本建立的功率激光社区收获(J-EPoCH)设施的概念设计相比较,该设施包括8千焦,5 PW@100赫兹激光。
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引用次数: 0
Process for Identifying QoS Requirements in the Multi-Domain Operations Environment 多域运行环境下QoS需求识别流程
Pub Date : 2022-04-05 DOI: 10.9766/kimst.2022.25.2.177
Dongsuk Park, Bong-ik Cho, Taehyung Park, Jaesung Lim
A network QoS model for the joint integrated C4I structure[1] was proposed for the integration of network infrastructure and network operations(NetOps) for NCOE. Detailed QoS requirements process of the joint integrated C4I systems are needs in the Multi-Domain Operation Environment(MDOE). A process is proposed for identifying QoS requirements and establishing in the MDOE using JMT(Joint Mission Thread) reference architecture and solution architecture. Mission analysis identify JCOAs(Joint Critical Operational Activities) and related activities based on JMT & System architecture's OVs, and Information analysis identify QoS attributes using System architecture's SVs. Identifying QoS attributes will be registered at PPS Registry by pre-regulated process, and will be set-up by NetOps. MDOE QoS requirement Process will support efficiently MUM-T and smart defense platform users under the future uncertain battlefield circumstances.
针对NCOE的网络基础设施与网络运营集成(NetOps),提出了一种面向联合集成C4I结构[1]的网络QoS模型。在多域作战环境下,联合集成C4I系统需要详细的QoS需求流程。提出了一个使用JMT(联合任务线程)参考体系结构和解决方案体系结构识别QoS需求并在MDOE中建立QoS需求的过程。任务分析基于JMT和系统体系结构的ov识别jcoa(联合关键作战活动)和相关活动,信息分析使用系统体系结构的SVs识别QoS属性。识别QoS属性将通过预先监管的过程在PPS注册中心注册,并由NetOps设置。MDOE QoS需求流程将在未来不确定的战场环境下有效支持MUM-T和智能防御平台用户。
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引用次数: 1
期刊
Journal of the Korea Institute of Military Science and Technology
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