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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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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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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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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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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Improved Finite Control Set Optimal Control for PMSM in Rocket Launcher Servo System by Di-fen Shi, Yuan-long Hou, Xiao-hui Gu, Run-min Hou

“…Permanent magnet synchronous motors (PMSMs) have been widely applied in the shipborne rocket launcher systems due to their high torque density and high efficiency. …”
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Peculiarities of archival information resources legal regulation in the field of research on the development of the rocket and space industry by L. M. Popova, А. V. Khromov

Subjects: “…rocket and space activities…”
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The Numerical Simulation Method of the Slot Crack Groups’ Effect Analysis for Solid Rocket Motor Grain by Tianpeng Li, Xiaonan Li, Zhaolong Xuan, Yu Guo

“…This study is aimed at the stability and effect of the crack groups in the solid rocket motor (SRM) grain when it was launched at normal temperature. …”
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Development and analysis of simulation of liquid-propellant rocket engine pump head curve obtaining process by D. A. Savchin, V. P. Nazarov

“…The paper describes the model of the centrifugal pump head curve obtaining process which helps in consideration of the implementation of automated systems in liquid-propellant rocket engine manufacturing. The work contains the simulation of automated and non-automated head curve obtaining. …”
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Chandail de hockey de Maurice « Rocket » Richard du Musée canadien des civilisations by Suzie-Anne Monast

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The position of liquid fuel residues in tank of worked-off rocket stage during ballistic descent by V. Yu. Kudentsov, A. V. Kudentsov

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Investigation of properties of system of automatic control of liquid-propellant rocket propulsion system with integrating regulator by I. A. Kyzmenko, A. B. Yakovlev

Subjects: “…liquid rocket engine…”
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Experimental Study of the Swirling Oxidizer Flow in HTPB/N2O Hybrid Rocket Motor by Mohammad Mahdi Heydari, Nooredin Ghadiri Massoom

“…Effects of swirling oxidizer flow on the performance of a HTPB/N2O Hybrid rocket motor were studied. A hybrid propulsion laboratory has been developed, to characterize internal ballistics characteristics of swirl flow hybrid motors and to define the operating parameters, like fuel regression rate, specific impulse, and characteristics velocity and combustion efficiency. …”
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Review of organizational value of science-intensive organizations configuration models (rocket and space industry organization case) by V. А. Shiboldenkov, S. S. Gavrilov

“…The article studies main models for compiling organizational cost of scientific-intensive enterprises used in rocket and space industry. Practical application of the most important value configurations analysis has been carried out, as well as analysis of economic activity. …”
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Development of mathematical model of processes in gas generator with unitary fuel for powering turbine of liquid rocket engine by A. B. Yakovlev

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