Acta Astronautica

Papers
(The H4-Index of Acta Astronautica is 39. The table below lists those papers that are above that threshold based on CrossRef citation counts [max. 250 papers]. The publications cover those that have been published in the past four years, i.e., from 2022-01-01 to 2026-01-01.)
ArticleCitations
Decreased human sperm motility and vitality after fast gravity load changes in a parabolic flight100
Thermite-for-demise (T4D): Experiments and numerical modelling on ball-bearing unit mock-ups containing thermite in an arc-heated wind tunnel92
Heating patterns and temperature distribution of projectile surface in lunar regolith penetration81
Publisher's note76
A deep neural network framework with Analytic Continuation for predicting hypervelocity fragment flyout from satellite explosions75
CerAMfacturing of a ceramic aerospike engine73
Evaluating sensor tasking strategies for object cataloging in GEO71
‘Sub-orbital activities’ – the application of ‘international law’ in the twilight between air and space law70
Towards a GNSS-assisted autonomous heterogeneous clock system for very small satellites in the Earth-Moon system69
Geometric analysis of a constellation with a ground target67
NASA's BioSentinel deep space CubeSat mission: successes and lessons learned66
Defining the notion of mining, extraction and collection: A step toward a sustainable use of lunar resources63
A reference implementation for knowledge assisted robot development for planetary and orbital robotics61
Trailing formations of lightweight spacecrafts to deflect NEAs by means of laser ablation60
Simulations of satellites mock-up fragmentation57
Development and characterization of the ECLIPS space environments simulation facility56
Guidance for autonomous spacecraft repointing under attitude constraints and actuator limitations55
Sun direction determination improvement by albedo input estimation combining photodiodes and magnetometer54
Adaptive control design for active Pogo suppression of large strap-on liquid launch vehicles51
Lunar highlands simulant — Geotechnical characterization, 3D discrete element modeling, and cone penetration simulations50
Relative orbit transfer using constant-vector thrust acceleration49
Self-deployable hinges for monolithic space structures using multi-material additive manufacturing49
Dynamics of jettison during Earth-to-NRHO transfers49
The use of detailed kinetics for modeling aerospace propulsion devices48
Lunar landing necessary building blocks and good practices for a sustainable development of human lunar activities47
Optimisation of a hybrid NS–DSMC methodology for continuous–rarefied jet flows46
PROBABILISTIC RISK ASSESSMENT (PRA) FOR ARTEMIS AND FUTURE SPACE EXPLORATION PROGRAMS46
Criteria for selection of point-ahead angle compensation strategy in intersatellite laser ranging interferometry of TianQin based on research of tilt-to-length coupling noise45
A Geospatial Artificial Intelligence and satellite-based earth observation cognitive system in response to COVID-1943
The Effects of Pointing Error Sources on Energy Delivery from Orbiting Solar Reflectors42
TWO-STAGE ‘slingshot amplifier’ can detect subtle gravitational deviations42
Optimization design and mechanism study of ion thruster performance based on CO2/xenon multi-propellant42
Spray angle prediction model for a multi-slit type throttleable gas–liquid pintle injector42
A Martian analog for spatially varying methane microseepage - polygons at Expedition Strip, Axel Heiberg Island41
Markers of distress among behavioral and physical health evacuees prior to emergency departure from Antarctica41
Determining the best technique: Methods, challenges, and innovations of performing microgravity CPR41
Geometric mechanics framework for tethered de-spinning of massive asteroids by small tug using passivity-based control40
Internal imaging of an extremely small-scale electron cyclotron resonance source revealing the formation of discharge mode transitions and hysteresis40
Three decades of ethological research in the space field within an interdisciplinary framework40
The technology platform of the EIVE CubeSat mission for high throughput downlinks at W-band39
Cost estimation for launch vehicle families considering uncertain market scenarios39
0.15663385391235