A comprehensive review of Electric Solar Wind Sail concept and its applications

M Bassetto, L Niccolai, AA Quarta, G Mengali - Progress in Aerospace …, 2022 - Elsevier
Abstract The Electric Solar Wind Sail (E-sail) is an innovative propellantless propulsion
system conceived by Pekka Janhunen in 2004 for use in interplanetary space. An E-sail …

Coulomb drag propulsion experiments of ESTCube-2 and FORESAIL-1

I Iakubivskyi, P Janhunen, J Praks, V Allik, K Bussov… - Acta Astronautica, 2020 - Elsevier
This paper presents two technology experiments–the plasma brake for deorbiting and the
electric solar wind sail for interplanetary propulsion–on board the ESTCube-2 and …

ESTCube-2 attitude determination and control: Step towards interplanetary CubeSats

I Ofodile, J Kütt, J Kivastik, MK Nigol… - 2019 IEEE …, 2019 - ieeexplore.ieee.org
Utilization of satellites to meet the needs of various missions requires a reliable Attitude
Determination and Control System (ADCS). In this paper, we presents a robust design of the …

[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 …

Trajectory approximation of a Coulomb drag-based deorbiting

L Niccolai, M Bassetto, AA Quarta, G Mengali - Aerospace, 2022 - mdpi.com
The presence of a number of space debris in low Earth orbits poses a serious threat for
current spacecraft operations and future space missions. To mitigate this critical problem …

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 …

Crowdfunding for satellite development: ESTCube-2 case

K Kalnina, K Bussov, H Ehrpais, T Teppo… - 2018 IEEE …, 2018 - ieeexplore.ieee.org
Here we present a successful crowdfunding campaign, which raised more than€ 38.7 k (≈
$45.8 k) for ESTCube-2 satellite development. Crowdfunding is the practice of funding a …

Optimal orbit transfer of single-tether E-sail with inertially fixed spin axis

AA Quarta, M Bassetto, G Mengali - Astrodynamics, 2024 - Springer
This study analyzes the optimal transfer trajectory of a spacecraft propelled by a spin-
stabilized electric solar wind sail (E-sail) with a single conducting tether and a spin axis with …

Electric sail phasing maneuvers for constellation deployment

L Niccolai, A Caruso, AA Quarta, G Mengali - Acta Astronautica, 2020 - Elsevier
The aim of this work is to investigate heliocentric phasing maneuvers performed by a
spacecraft propelled by an Electric Solar Wind Sail, that is, an innovative propellantless …

Rapid evaluation of the decay time of a plasma brake-based CubeSat

M Bassetto, L Niccolai, AA Quarta, G Mengali - Aerospace, 2022 - mdpi.com
The plasma brake is a propellantless device conceived for de-orbiting purposes. It consists
of an electrically charged thin tether that generates a Coulomb drag by interacting with the …