Acta Astronautica : Impact Factor & More

An ultra-compact mechanical interface universal design for orbital replacement unit

Corrigendum to ‘Orbit determination for spacecraft with continuous low-thrust using nonsingular Thrust-Fourier-Coefficients and filtering-through approach’ [Acta Astronaut. 224 November 2024, 353–366, AA_10602]

Improving landing stability and terrain adaptability in Lunar exploration with biomimetic lander design and control

Effects of pulse injection on the flow field structure and combustion performance in a kerosene-fueled supersonic combustor

Orbital motion control of an electrically charged spacecraft

Characterization of the outgassing event during BepiColombo second Venus flyby using Italian Spring Accelerometer data

An ultra-compact mechanical interface universal design for orbital replacement unit

Corrigendum to ‘Orbit determination for spacecraft with continuous low-thrust using nonsingular Thrust-Fourier-Coefficients and filtering-through approach’ [Acta Astronaut. 224 November 2024, 353–366, AA_10602]

Improving landing stability and terrain adaptability in Lunar exploration with biomimetic lander design and control

Effects of pulse injection on the flow field structure and combustion performance in a kerosene-fueled supersonic combustor

Orbital motion control of an electrically charged spacecraft

Characterization of the outgassing event during BepiColombo second Venus flyby using Italian Spring Accelerometer data