Unsteady flow and heat transfer optimization of viscous fluid with bioconvection over a rotating stretchable disk and gyrotactic motile microorganisms by Mazhar Hussain, Samya Shahid, Noreen Sher Akbar, Mohammed Kbiri Alaoui

“…Graphical results indicates that parameters like increment of unsteady effects helps in dissipation of thermal energy rapidly and bioconvection evidently influenced velocity, temperature and microorganism profile by thinning the microorganism layer, showing valuable results for optimizing thermal systems like in aerospace engineering where spacecraft undergo extreme temperature due to friction between spacecraft and atmosphere.…”
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Vibration Feedforward Compensation for Magnetically Suspended Control and Sensitive Gyroscope with Spherical Rotor by Qiang Liu, Heng Li, Cong Peng, Sha Sheng, Zhaojing Yin, Zhiguo Liu

“…The spacecraft attitude can be sensed by a high-speed rotor without deflection interference torque. …”
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FEATURES OF CONSTRUCTION REMOTE SENSING IMAGING SPECTROMETERS FROM SPACE by N. K. Artyukhina, M. N. Kotov

“…In article factors influencing quality of the Earth image received with imaging spectrometers are presented: height of an orbit of a spacecraft, atmosphere, characteristics of the optical scheme, type of dispersive element and a photodetector. …”
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Investigation on Computing Method of Martian Dust Fluid Based on the Energy Dissipation Method by Tianxiang Ding, Xuyan Hou, Man Li, Guangyu Cao, Jixuan Liu, Xianlin Zeng, Zongquan Deng

“…This model is based on the existing DMT model to analyze the collision deposition of dust fluid particles, including particle-spacecraft collision and particle-particle collision. …”
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Propellant Slosh Force and Mass Measurement by Andrew Hunt, Richard Foster-Turner, Ross Drury

“…Fully instrumented Smart Tanks will be able to provide force vector inputs to a spacecraft inertial navigation system; this in turn will (i) eliminate or reduce navigational errors, (ii) reduce wait time for uncertain slosh settling, since actual slosh forces will be known, and (iii) simplify slosh control hardware, hence reducing overall mass. …”
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Microstructures and tensile properties of Mg-2Zn-0.8Sr-0.2Ca alloy extruded at relatively slow speed and low temperature by Yang A., Nie K.-B., Deng K.-K., Han J.-G., Xiao T., Han X.-Z.

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Behavior of a Free Dual-Spin Gyrostat with Different Ratios of Inertia Moments by Vladimir Aslanov

“…The results of the study can be useful for the analysis of dual-spin spacecraft dynamics.…”
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Hearing Loss in Space Flights: A Review of Noise Regulations and Previous Outcomes by Ahmet Uğur Avcı

“…Certain precautions must be taken to ensure the habitability of the spacecraft and prevent potential hearing loss in astronauts or space flight participants. …”
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Electron Acceleration by Multiple Fast Fermi Reflections at Earth’s Bow Shock by Y. Y. Liu, J. B. Cao, C. M. Liu, Y. T. Song, D. K. Hu

“…Using measurements from the Magnetospheric Multiscale spacecraft, we report unexpected spiky enhancements of energetic electron flux in the upstream region of the Earth’s bow shock. …”
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Academician V. H. Serheiev – Control System Designer, Founder of the Scientific and Design School, Honored Citizen of Kharkiv (on His 110th Birthday) by Elena Tverytnykova, Olena Voitiuk

“… March 5, 2024 marks the 110th birthday of Volodymyr Hryhorovych Serheiev, an outstanding scientist, chief designer of control systems for strategic combat missiles, launch vehicles, spacecraft and transport modules of orbital complexes, Academician of the National Academy of Sciences of  Ukraine and an Honored Citizen of Kharkiv. …”
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Propagation of Interplanetary Shocks in the Inner Heliosphere by Munkhjargal Lkhagvadorj, Gábor Facskó, Andrea Opitz, Péter Kovács, David G. Sibeck

“…During the 2007 May 7 event, the shock parameters and the shock normal direction remain consistent across each spacecraft crossing of the shock. The shock surface appears to be tilted by almost the same degree as the Parker spiral, and the driver could be a corotating interaction region (CIR). …”
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Low-Thrust Transfer Design of Low-Observable Geostationary Earth Orbit Satellite by Bing Hua, Zhujun Shao

“…With radar and surface-to-air missiles posing an increasing threat to on-orbit spacecraft, low-observable satellites play an important role in low-thrust transfers. …”
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Implementation of Surface Radiation and Fluid-Structure Thermal Coupling in Atmospheric Reentry by Ojas Joshi, Pénélope Leyland

“…In this paper, we investigate how the thermal radiation coming from the postshock region interacts with the spacecraft structure. A model that takes into account the radiation reflected by the surface is developed and implemented in a solid solver. …”
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30 years of CNES parabolic flights for the benefit of the scientific community by Rouquette, Sébastien

“…The use of parabolic flights is complementary to other microgravity carriers, and preparatory to manned space missions onboard the International Space Station and other manned spacecraft, around the Earth or beyond, to the Moon for example.The main advantages of parabolic flights for microgravity investigations are the short turn-around time, the relatively low cost, the flexibility of experimental approach, the possibility of direct intervention by investigators on board the aircraft during and between parabolas, and the possibility of modifying the experiment set-up between flights.…”
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Consensus control of multi-agent systems with delays by Yi Gong

“…Consensus control is widely applied in spacecraft formation, sensor networks, robotic manipulators, autonomous vehicles, and others. …”
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A New Method to Improve the Measurement Accuracy of Autonomous Astronomical Navigation by Yu-Feng Yang, Xiang Han, Ning-Ning Song, Zi-Chen Wang

“…The atmospheric temperature and density model with space-time variation is constructed. The spacecraft state equation and the measurement equation with the starlight apparent height as the observation quantity are established. …”
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Artificial Controlling of the Collinear Liberation Points Using Lorentz Force in the Restricted Three-Body Problem by M.I. El-Saftawy, M.A. Yousef, A. Mostafa

“…This work studies the possibility of generating artificial collinear liberation points for the planar circular restricted three-body problem using Lorentz force affecting a charged spacecraft due to the magnetic field of a planet. It is considered to be a magnetic dipole inclined by angle α with the spin axis of the planet. …”
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Real-Time Optimal Approach and Capture of ENVISAT Based on Neural Networks by Hongjue Li, Yunfeng Dong, Peiyun Li

“…A neural network-based controller is developed to enable a chaser spacecraft to approach and capture a disabled Environmental Satellite (ENVISAT). …”
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Brine-Induced Tribocorrosion Accelerates Wear on Stainless Steel: Implications for Mars Exploration by Javier Martín‐Torres, María‐Paz Zorzano‐Mier, Erik Nyberg, Abhilash Vakkada-Ramachandran, Anshuman Bhardwaj

“…Although corrosive chemical species such as materials like chloride atoms, chlorides, and perchlorates have been detected on the Martian surface, there is a lack of studies of its impact on materials for landed spacecraft and structures that will support surface operations on Mars. …”
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Numerical Simulation for Thermal Shock Resistance of Thermal Protection Materials Considering Different Operating Environments by Weiguo Li, Dingyu Li, Ruzhuan Wang, Daining Fang

“…Based on the sensitivities of material properties to temperature and the complexity of service environment of thermal protection system on the spacecraft, ultrahigh-temperature ceramics (UHTCs), which are used as thermal protection materials, cannot simply consider thermal shock resistance (TSR) of the material its own but need to take the external constraint conditions and the thermal environment into full account. …”
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