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ABSTRACT
- An experimental study on the cracking heat sink behavior of n-decane and RP-3 under supercritical pressures
- Design optimization and regulation mechanism of channel configuration for a radial wave rotor combustor
- Aerodynamic Impact of Protuberance-Induced Thrust Vectoring in Supersonic C-D Beveled Nozzles: A Comprehensive Experimental and Numerical Approach
- On-orbit demonstration of near real-time communication via Globalstar for time-domain astronomy
- Lunar Landing and Launching Pad Design Considerations Using ISRU Materials
- THE RAMON SPACE RACE PROGRAM: EMPOWERING TEACHERS FOR EARLY CHILDHOOD SPACE EDUCATION
- Modeling of the Macro-Scale Nanostructured Multilayer Membranes in the Rarefied Atmospheres for Multiple Planets
- Dual hybrid non-fragile control for integrated electromagnetic docking and separation of spacecraft
- KPLO’s Conjunction Mitigation in Lunar Orbit: Operational Results and Strategic Insights from International Collaboration
- LunarLeaper—A mission concept to explore the lunar subsurface with a small-scale legged robot
- Blood coagulability changes in females exposed to dry immersion: examining a mechanism for the development of venous thromboembolism in microgravity.
- RISK KNOWLEDGE IMPROVEMENT FROM ADDITIONAL INFORMATION FOR THE PDC25 HYPOTHETICAL IMPACT SCENARIO
- A model for the estimation of freestream Mars horizontal wind speeds and directions for MEDA wind sensors in NASA-JPL Mars 2020 mission. Part I: Aerodynamic modeling of Perseverance boundary layer using CFD.
- A description of plume-surface interactions and non-dimensional analysis for crater formation
- Comments on “Space sustainability via flexible controlled expandable net for multiple irregular debris removal”
- Monitoring the Radiation Environment in High-Latitude Low-Earth Orbit During an Ascending Phase of the Solar Cycle (July 1, 2023 to July 31, 2024)
- Research of an optical method for determining the mutual positioning of microsatellites to ensure the safety of a low- orbital constellation
- Artificial Intelligence-Powered Space Systems Including Launch, Space, Ground and User Segments: Current Status and Future Challenges
- Global optimization of space mission concept of operations and systems design via mixed-integer nonlinear programming
- Approach strategies for inserting into Enceladus science orbit configurations
- Integrated Control System Functions for Enhancing Take-off and Landing Safety of Aerospace/High Speed Flying Vehicles
- Possibilities and limitations of thermal infrared detections of the Chelyabinsk progenitor and 2024 YR4 before Earth encounters
- NEO and imminent impactor discoveries from Hungary: Recent results and lessons learnt
- A setup to test high altitude and astronaut helmets on blast and shock wave mitigation
- Study on combustion instability induced by resonance self-excited whistling in pipe
- Information manifold of space target maneuver detection systems in view of relative orbital motion
- Analytical synthesis of control laws for longitudinal motion of an aircraft-type spacecraft at incomplete information on the state vector
- Numerical modeling of thermal loading of composite aerospace vehicle parts containing cracks
- Modelling vibrational segregation of granular materials in lunar gravity using the discrete element method
- Laser Directed Energy Deposition Additive Manufacturing of Lunar Regolith Simulant
- Multiple Aspects of Preserving Lunar Space Heritage
- LISA drag-free attitude control system: Robust stability and performance analysis
- Flame Stabilization Mode Transitions in Supersonic Combustion of Liquid Kerosene with Gas-Assisted Atomization
- Effects of inflow total pressure on combustion performance of kerosene-fueled multi-cavity scramjet combustor
- HA-PointAE: A Novel Hybrid Attention PointNet Autoencoder for High-Fidelity Airfoil Generation and Aerodynamic Shape Optimization
- Residual Learning Method for Mars Aerobraking Autonomous Predictive Guidance
- Influence of ionization processes on thermoelectric detector readings at measuring heat fluxes in shock tubes
- Dynamic modeling, flight control design, and simulation verification of a Ring-Wing Tail-sitter UAV with rudder and propeller redundancy actuator
- Mission Planning for UAV Swarm Air-Launched by Single Carrier Aircraft under Multiple Constraints
- Pulsed Guidance Method for Exo-Atmospheric Interceptor via Reinforcement Learning
- Topology Optimization Framework for Designing Elastic Wind Tunnel Models with Additive Manufacturing
- The limits of high-temperature accommodation of cesium and strontium by protective coatings of spacecraft for radiation background reduction during space missions
- Characterization of horizon-based optical navigation measurement errors around the Moon: Patterns, their evolution, and a modeling approach
- Enrichment of the driving metanarratives shared between SETI and space sustainability through a multispecies lens
- Failure Phenomena and Mechanisms in the Wave Rotor-Combustor Closed Loop System
- Local blade profiling design for stall-stage rotor in a three-stage compressor: a numerical investigation using dissipation weighting
- Forgetting filter-based real-time identification and compensation of whole-angle hemispherical resonator gyroscope errors for extensive aerospace applications
- Experimental and CFD investigation of the heat flux distribution and flow field structure on the leeward side of a 75∘ delta flat plate
- RB-LLM Control: an Intelligent Control Framework with Rule-Based Large Language Model Decision-Making
- Thermal control mode of an active phased antenna array using modified Fourier series in the presence of rapidly changing thermal flows over time
- The influence of the periodic longitudinal concentration gradient on the detonation re-initiation behind the pre-detonation tube
- Vostochny Cosmodrome: Crew emergency rescue scenarios
- Analytical approximation of the propulsion dynamics of magnetic sail with fixed solar incidence angle
- Twin Parallel Mechanisms for Aerospace Deployable Structures
- Efficient Real-Time Reconstruction of Transient Temperature Fields in Some Hypersonic Thermal Protection Systems with a Conditioned Adaptive Physics Network
- A time-efficient method for dynamic analysis of rotating composite blisk based on referenced nodal coordinate formulation
- Taxiway path planning at airports based on dynamic directed graphs and DQN
- An End-to-End Deep Learning Framework for Separation and Parameter Measurement of Composite Intermittent Sampling Repeater Jamming
- Envelope parameter sensitivity analysis on fluid-thermal-structural coupling characteristics of stratospheric non-rigid airship
- Mission specific PID tuning for energy-efficient quadrotor flights
- Surrogate-assisted evolutionary optimization and microgravity experimental validation of a planar deployable mechanism
- Stability Boundaries and Nonlinear Aeroelastic Behavior of a Supersonic Panel under Thermal-Degradation and Damping Effects
- Test and numerical simulation study on the containment characteristic of an aeroengine turbine casing
- Long-Term Multi-Region Observation Scheduling for Large-Scale Constellations via Two-Stage Hybrid Planning
- A framework for flight vehicle aerodynamic data fusion based on generative models and interpretability methods
- Transient Evolution of Flow Structures Induced by Sweeping Jets on a Circular Cylinder via Multi-Scale Proper Orthogonal Decomposition(mPOD)
- DCR-YOLO: An enhanced anti-UAV detection method based on triple collaborative optimization strategy
- Semantic-Aware Visual Localization for Robust Aerial Perception
- Conceptual Design and Analysis of a Tube-Launched Fixed-Wing UAV with Integrated Folding Wing Systems
- Flow Instability Analysis of Interactions Between Regenerative Cooling Channels with Lateral Non-uniform Heating
- Vortex Dynamics and Propulsion Efficiency of Pulsed Laval Nozzles Investigated by Large Eddy Simulation
- Design and optimization of a tubular combustor for supersonic propulsion using genetic algorithms
- Hybrid Slime Mould Algorithm for Efficient Optimization of Chemical Kinetic Mechanisms in Scramjet Turbulent Combustion Simulations
- Designing complex re-entrant honeycombs with optimal auxeticity
- Robust thruster-only constrained optimal slew control strategies for nanosatellites
- Nonlinear aeroelastic analysis of an all-movable horizontal tail with bending free-play
- Design and analysis of a bistable capture mechanism based on ring deployable scissor linkages
- Numerical and experimental exploration on the strut-cavity flow characteristics induced by the oblique shock wave in supersonic crossflow
- Lightweight machine learning approaches for modeling a rotating cavity with vortex-reducing tubes
- Study on the mechanism of inhibiting the deterioration of compressor performance caused by interstage leakage using root slots
- Investigation of loss mechanisms inside ultra-highly loaded transonic tandem compressors with different critical design parameters
- Air route network planning for urban logistics with vertihub: An airspace model
- Fuel-optimal low-thrust gravity-assist trajectory optimization using sequential convex programming and adaptive mesh refinement
- Multi-Unit hybrid modeling method and nonlinear dynamics analysis of the whole aero-engine system
- Numerical investigations on aerodynamic characteristics in a longitudinal V-shaped hypersonic vehicle formation
- Deep reinforcement learning-based fast hybrid planning for multi-type on-orbit service under mass variation dynamics
- Nonlinear group and phase velocity analysis and architectural design of functionally graded tapered plates under supersonic airflow
- Planar laser-induced fluorescence visualization of microporous-wall seeping gas films in supersonic boundary layers
- Predefined-time trajectory tracking control of a rigid-flexible cable-driven space manipulator using neural network
- Safe reinforcement learning based agile satellite attitude control for non-cooperative target tracking with operation constraints and actuator faults
- Improving the hydrogen-oxygen combustion efficiency of cavity-based scramjet by ionizing hydrogen
- Uncertainty propagation of spacecraft orbits around asteroid 99942 Apophis using a hybrid MGMM-UT approach
