Analysis of Load Optimization in Solid Rocket Motor Propellant Grain with Pressure Cure by Zhanxin Cui, Haiyang Li, Zhibin Shen, Huiru Cui

“…This technology can effectively reduce the risk of damage to the structural integrity of the grain in the case-bonded casting solid rocket motor. In this paper, ABAQUS is used to establish a finite element model of star-shaped grains. …”
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Load Characteristics and Modeling Methods for the Flow Regulator of a Solid Ducted Rocket by An Wang, Qinghua Zeng

“…The load characteristics for the flow regulator of a solid ducted rocket are discussed in this paper. The mechanism and the influence factor of the load in the flow regulator were studied both theoretically and experimentally, and the system load and the working load were divided according to the mechanism. …”
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Buckling Instability of Flexible Joint under High Pressure in Solid Rocket Motor by Wang Chunguang, Xu Guiyang, Gong Jianliang

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Using Hydrogen Peroxide for Rocket Fuel Tank Pressurization: Innovations, Advantages, and Challenges by Mykhailo Vorobei, Mykola Bondarenko

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Fault-Tolerant Guidance of Rocket Vertical Landing Phase Based on MPC Framework by Jingqi Li, Yaosong Long, Mao Su, Lei Liu, Bo Wang, Zhongtao Cheng

“…For the vertical landing process of reusable rockets, the landing accuracy is likely to be affected by disturbances and faults during flight. …”
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SIMULATION ANALYSIS AND GROUND TEST OF SOLID ROCKET MOTOR GRAIN WITH SURFACE CRACK by LI Fei, XIAN Yong, ZHI ShiJun

Subjects: “…Solid rocket motor…”
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A Multiconstrained Ascent Guidance Method for Solid Rocket-Powered Launch Vehicles by Si-Yuan Chen, Qun-Li Xia

“…This study proposes a multiconstrained ascent guidance method for a solid rocket-powered launch vehicle, which uses a hypersonic glide vehicle (HGV) as payload and shuts off by fuel exhaustion. …”
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FREQUENCY PREDICTION OF STAGED COMBUSTION ROCKET ENGINE BASED ON RBF NEURAL NETWORK by DU FeiPing, TAN YongHua, CHEN JianHua

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Thermal Structure Strength Analysis of Nozzle of Solid Rocket Motor with the Coupled Algorithm by Chunguang Wang, Weiping Tian, Kaining Zhang

“…In order to achieve the thermal structural integrity analysis of the solid rocket motor nozzle accurately and efficiently, the multifield (flow-thermal-mechanical) coupled numerical investigation was carried out based on the mesh-based parallel code coupled interface. …”
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Experimental studies of unsteady processes of cryogenic liquid evaporation in rocket tank model by V. I. Trushlyakov, V. A. Urbansky, A. N. Pavlenko, V. E. Zhukov, E. Yu. Sukhorukova

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A Concept for Striking Range Improvement of the GROM/PIORUN Man-Portable Air-Defence System by Krzysztof MOTYL, Mirosław MAKOWSKI, Bogdan ZYGMUNT, Zbigniew PUZEWICZ, Janusz NOGA

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Numerical Simulation of Coupling Thermal and Mechanical Influence on Submerged Nozzle in Solid Rocket Motor by Jian-Liang Gong

“…The coupling thermal and mechanical effect on submerged nozzles is important in the design of modern rockets upon thermal loading and aerodynamic pressure. …”
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Research on the efficiency of rocket mine laying under the different wind speed and wind direction by TU Jiangang, WANG Wei, ZHAO Kuisheng, CHEN Shi

“…In this paper, a model for evaluating the operational efficiency of rocket mine laying bomb is established, the relationship between wind speed and wind direction and the landing position of rocket mine laying bomb is simulated and analyzed. …”
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DESIGN AND STRESS ANALYSIS OF RX-122 ROCKET MOTOR TUBE USING NUMERICAL METHOD by Lasinta Ari Nendra Wibawa, Iyus Rusyana, Dinar Koswara, Gagan Nugraha, Diyat Muhdiyat, Dedi Irawan

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Quality Diagnosis for Rocket Body Structure Manufacturing Process Based on Product Quality DNA by Yao Jiayu, Liu Haijiang

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Strain Prediction of Grain in Solid Rocket Motor under the Pressure Curing Molding Technology by Kaining Zhang, Chunguang Wang, Qun Li, Zhenyu Guo

“…The residual strain generated in grains during the propellant manufacturing process can significantly impact the safety and stability of solid rocket motors. Pressure curing molding technology has been employed as an effective approach to mitigate residual strain. …”
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Ignition and Flame Stabilization of a Strut-Jet RBCC Combustor with Small Rocket Exhaust by Jichao Hu, Juntao Chang, Wen Bao

“…A Rocket Based Combined Cycle combustor model is tested at a ground direct connected rig to investigate the flame holding characteristics with a small rocket exhaust using liquid kerosene. …”
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Simulation Analysis of Vibration and Noise Characteristic of Rocket Artillery Elevating Mechanism Planetary Reducer by Li Zhigang, Wang Zhengyao

“…A foundation for further understand the dynamic performance of the rocket artillery elevating mechanism reducer is provided,and the technical support for the optimal design of vibration and noise reduction of this sort of reducer is also provided.…”
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Research on the Connection of Heterogeneous Non-Metallic Materials in the Manufacture of Rocket and Space Technology Structures by Tamara Manko, Krystyna Kozis

“… In order to choose a method of joining dissimilar non-metallic materials in the manufacture of compartments of rocket and space technology, it is of particular interest to study the adhesion strength using a whole range of materials. …”
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A Model for Igniter Mass Flow Rate History Evaluation for Solid Rocket Motors by Yanjie Ma, Futing Bao, Weihua Hui, Yang Liu, Yijie Gao

“…Although derived on the basis of a small-scale solid rocket motor, the model has the potential to be used in large-scale systems.…”
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