The analysis of features of occurrence of inertial explosion in problems of high-speed impact of metal penetrators into the studied celestial body and meteor-technogenic particles into elements of spacecraft by E. V. Leun, D. B. Dobriza, А. А. Poliakov, V. К. Sysoev

“…The article discusses the features of the occurrence of an inertial explosion (IE) in the problems of high-speed impacts on a solid barrier of two types of impactors: metal penetrators into the studied celestial body for space contact scientific research and meteor-technogenic particles into the elements of spacecraft. The features of IE, the conditions of its occurrence and the results of theoretical and experimental studies are analyzed. …”
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Two-gaps microwave ion engine and its study by aerodynamic method by I. S. Vavilov, P. S. Yachmenev, V. V. Fedyanin, K. I. Zharikov, P. V. Stepen, A. I. Lukyanchuk, I. A. Kuzmenko

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Calorimetric studies of microwave ion thruster by I. S. Vavilov, K. I. Zharikov, P. S. Yachmenev, V. V. Fedyanin, P. V. Stepen, A. I. Lukyanchuk, I. A. Kuzmenko

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Design of CubeSat-Based Multi-Regional Positioning Navigation and Timing System in Low Earth Orbit by Georgios Tzanoulinos, Nori Ait-Mohammed, Vaios Lappas

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The analysis of the state of development of devices for cleaning orbits in near-Earth space from large-sized space debris objects by V. I. Trushlyakov, V. V. Yudintsev, V. A. Urbansky, S. Yu. Onishchuk

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The method of investigation of basic project parameters of microsatellite by random search by V. N. Blinov, A. I. Lukyanchik, V. V. Shalay

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The radiation from ultrafast point dipoles, moving uniformly near chiral media by V. N. Kadantsev

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Quality control of metallized polymer films after automated laser perforation by P. A. Vyatlev, E. V. Leun, D. V. Sergeev, V. K. Sysoev

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TRAINING OF ENGINEERS USING THE PROJECT-ORIENTED TEACHING by Igor V. Kovalev, Yuriy Y. Loginov, Pavel V. Zelenkov

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Research and Verification of Key Techniques in the Simulation of Space Extremely Rapid Decompression in Millisecond by Junwei Wang, Lei Zhang, Guohua Li, Ran Liu, Juan Ning, Xiao Han, Xin He

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Effect of Feature Size on Defects, Microstructure, and Mechanical Properties of Selective Laser Melted AlSi10Mg Lattice Structure by Chengkuan Peng, Junfeng Qi, Sheng Zhou, Sanqiang Yang, Ran Tao, Heng Shao, Weining Li

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Thermomechanical Fatigue of Unidirectional Carbon Fiber/Epoxy Composite in Space by Ali Anvari

“…Thermomechanical fatigue is one of the challenges for spacecrafts during space missions. As a result of the extreme temperature variation in space, thermal cycles are created, and due to the imposed mechanical loads to spacecrafts such as engine loads while they turn on and off, mechanical cycles are created. …”
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Thermal modeling and empirical verification of multi unit small satellites by Anwar Ali, Muhammad Rizwan Mughal, Shoaib Ahmed Khan, Kar Seng Teng

“…The proposed model is a useful tool for the preliminary design phase of a spacecraft design. By utilizing the proposed model, the designer can determine the type of material and its dimensions that can be used to obtain low thermal resistance of the spacecraft structure.…”
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Space mission as a service (SMaaS): General-purpose computing on space by Leonardo Camargo-Forero, Julián G. Rodríguez-Ferreira, Carlos J. Barrios-Hernández

“… Given the critical nature of their missions, space systems such as satellites, probes, spacecraft, etc., are commonly embedded with specific hardware and software solutions. …”
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Development of an Anchoring System for the Soft Asteroid Landing Exploration by Zhijun Zhao, Shuang Wang, Delun Li, Hongtao Wang, Yongbing Wang, Jingdong Zhao

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Expandable Orbit Decay Prediction Using Continual Learning by Junhua He, Hua Wang, Haitao Wang, Xuankun Fang, Chengyi Huo

“…Very low earth orbit (VLEO) spacecraft have become an attractive proposition with obvious advantages in various missions, including communication and ground observation. …”
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Robust Onboard Orbit Determination Through Error Kalman Filtering by Michele Ceresoli, Andrea Colagrossi, Stefano Silvestrini, Michèle Lavagna

“…Accurate and robust on-board orbit determination is essential for enabling autonomous spacecraft operations, particularly in scenarios where ground control is limited or unavailable. …”
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Application of Wave Propagation to Pyroshock Analysis by M. Gherlone, D. Lomario, M. Mattone, R. Ruotolo

“…Pyroshocks are high frequency transients due to pyrotechnic devices used in aerospace engineering in order to deploy solar arrays and antennae, separate subsystems from the spacecraft or separate the spacecraft itself from the base stage booster; their prediction is usually complex and very time consuming.…”
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Detecting Silent Data Corruptions in Aerospace-Based Computing Using Program Invariants by Junchi Ma, Dengyun Yu, Yun Wang, Zhenbo Cai, Qingxiang Zhang, Cheng Hu

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A Novel Analytical Inverse Kinematics Method for SSRMS-Type Space Manipulators Based on the POE Formula and the Paden-Kahan Subproblem by Yecong Wang, Xilun Ding, Zixin Tang, Chengwei Hu, Qingqing Wei, Kun Xu

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