ACTA ASTRONAUTICA Journal

Overview

abbreviation

ACTA ASTRONAUT

publication venue for

Bare Photovoltaic Tether characteristics for ISS reboost. 229:34-42. 2025
Fast recovery mode for micro-meteoroid impacts: A LISA mission study. 229:199-210. 2025
Simulator and hardware emulator of a short electrodynamic tether system. 226:298-308. 2025
A review of electrodynamic tether missions: Historical trend, dimensionless parameters, and opportunities opening space markets. 225:158-168. 2024
Multi-disciplinary optimization of constellation deployment strategies including launcher selection. 223:389-403. 2024
Optimal design and current control strategies of an electrodynamic tape for ISS station-keeping. 223:621-629. 2024
Strategies for hollow cathode command in short electrodynamics tether-based deorbit devices. 222:1-10. 2024
Computational studies on hyper velocity impact of spherical projectiles on whipple shield with hybrid Newtonian fluid-filled core. 220:230-242. 2024
Emission and performance characterization of ionic liquids for an externally wetted electrospray thruster. 219:97-107. 2024
Deflection of dangerous middle-size LEO debris with autonomous space-based laser brooms via surgical actions. 217:75-88. 2024
Numerical Analysis of Hyper Velocity Impact on quasi-isotropic carbon fiber reinforced polymer laminates. 217:323-332. 2024
An electric model for bare-photovoltaic tethers in the passive mode. 214:609-618. 2024
A filter for tracking non-cooperative low-thrust satellites using surveillance radar data. 213:694-707. 2023
Impact of propellant temperature on the emission regime of an externally wetted electrospray system using time-of-flight mass spectrometry. 213:145-155. 2023
Performance characterization of the µ10 electron-cyclotron-resonance ion thruster using alternative propellants: krypton vs. xenon. 211:750-754. 2023
Cross-verification and benchmarking analysis of electrodynamic tether simulators. 208. 2023
Guidance for autonomous spacecraft repointing under attitude constraints and actuator limitations. 207:340-352. 2023
Post-Newtonian corrections to JCA. 201:p. 172-p. 181. 2022
A code for the analysis of missions with electrodynamic tethers. 198:471-481. 2022
Validation of enabling technologies for deorbiting devices based on electrodynamic tethers. 198:707-719. 2022
Satellite maneuver detection and estimation with radar survey observations. 201:p. 274-p. 287. 2022
Attitude determination and control for the deployment preparation phase of a space tether mission. 193:381-394. 2022
Trailing formations of lightweight spacecrafts to deflect NEAs by means of laser ablation. 190:241-250. 2022
Three-dimensional neutralizer effects on a Hall-effect thruster near plume. 187:498-510. 2021
Launcher Flight Control Design using Robust Wind Disturbance Observation. 186:303-318. 2021
A bare-photovoltaic tether for consumable-less and autonomous space propulsion and power generation. 180:350-360. 2021
The E.T.PACK project: Towards a fully passive and consumable-less deorbit kit based on low-work-function tether technology. 177:821-827. 2020
Tethers in space. 177:749-749. 2020
Trade-off analysis of C12A7: e-deposition techniques applied to Low Work Function Tethers. 177:806-812. 2020
Hybrid multi-objective orbit-raising with operational constraints. 175:447-461. 2020
Three-dimensional geomagnetic field effects on a plasma thruster plume expansion. 175:190-203. 2020
Systematic performance-oriented guidance tuning for descent & landing on small planetary bodies. 158:44-54. 2019
Trajectory design and guidance for landing on Phobos. 151:389-400. 2018
Spacecraft-plasma-debris interaction in an ion beam shepherd mission. 146:216-227. 2018
Post-Newtonian equations of motion for LEO debris objects and space-based acquisition, pointing and tracking laser systems. 141:132-142. 2017
A Cartesian relative motion approach to optimal formation flight using Lorentz forces and impulsive thrusting. 140:255-263. 2017
Autonomous shooting at middle size space debris objects from space-based APT laser systems. 131:83-91. 2017
Determination of the force transmitted by an ion thruster plasma plume to an orbital object. 119:241-251. 2016

International Standard Serial Number (ISSN)

0094-5765

Electronic International Standard Serial Number (EISSN)

1879-2030