Thrust model and guidance scheme for single-tether E-sail with constant attitude

M Bassetto, AA Quarta, G Mengali - Aerospace Science and Technology, 2023 - Elsevier
In its typical arrangement, an Electric Solar Wind Sail (or E-sail) consists of a grid of long
tethers charged by means of a high-voltage source that creates an electrostatic sheath …

Electric sail mission expeditor, ESME: Software architecture and initial ESTCube lunar cubesat E-sail experiment design

MF Palos, P Janhunen, P Toivanen, M Tajmar… - Aerospace, 2023 - mdpi.com
The electric solar wind sail, or E-sail, is a novel deep space propulsion concept which has
not been demonstrated in space yet. While the solar wind is the authentic operational …

[HTML][HTML] Advances in CubeSat Sails and Tethers

A Slavinskis, P Janhunen - Aerospace, 2024 - mdpi.com
Currently, most space missions rely on chemical and electric propulsion systems, both of
which are limited by the propellent tank volume whose “wet mass” is launched from the …

Warm start for optimal transfer between close circular orbits with first generation E-sail

AA Quarta - Advances in Space Research, 2025 - Elsevier
Abstract The Electric Solar Wind Sail (E-sail) is a propellantless propulsion system for deep
space navigation that exploits the dynamic pressure of the solar wind to generate thrust …

Performance Estimate of a Spin-Stabilized Drag Sail for Spacecraft Deorbiting

L Niccolai, G Mengali - Applied Sciences, 2024 - mdpi.com
The growing amount of space debris in geocentricorbit poses a significant threat to the future
of space operations. To mitigate this problem, current international guidelines state that a …

Trends and Applications of On-Board Image Processing for Earth Observation Nanosatellites: A Systematic Review

MA Chanoui, I Khalil, M Sbihi… - International Journal of …, 2025 - Springer
On-board image processing represents a practical application for satellite imagery, aiming to
optimize or prioritize data transmission to ground stations, thereby enhancing bandwidth …

[HTML][HTML] Low-cost MPPT for triple-junction solar cells used in nanosatellites: a comparative study between P&O and INC algorithms

A Lemmassi, A Derouich, A Hanafi, A Byou… - e-Prime-Advances in …, 2024 - Elsevier
This paper presents a study of solar panels composed of triple-junction solar cells used in
CubeSats; in particular, it focuses on optimizing the power supplied by these panels using …

[HTML][HTML] Decay time estimate for LEO spacecraft

L Niccolai, G Mengali - Acta Astronautica, 2024 - Elsevier
The growing concerns posed by orbital debris represent a serious threat to the future of
space operations in low Earth orbit. With the goal of limiting the formation of new debris …

[HTML][HTML] Impact of Pitch Angle Limitation on E-Sail Interplanetary Transfers

AA Quarta - Aerospace, 2024 - mdpi.com
The Electric Solar Wind Sail (E-sail) deflects charged particles from the solar wind through
an artificial electric field to generate thrust in interplanetary space. The structure of a …

Optimal Guidance for Heliocentric Orbit Cranking with E-Sail-Propelled Spacecraft

AA Quarta - Aerospace, 2024 - mdpi.com
In astrodynamics, orbit cranking is usually referred to as an interplanetary transfer strategy
that exploits multiple gravity-assist maneuvers to change both the inclination and eccentricity …