[HTML][HTML] Обзор и выбор средств увода крупногабаритного космического мусора
РС Пикалов, ВВ Юдинцев - Труды МАИ, 2018 - cyberleninka.ru
В работе рассматриваются способы активной очистки околоземных орбит от
крупногабаритного космического мусора. Представлена классификация способов увода …
крупногабаритного космического мусора. Представлена классификация способов увода …
Active space debris removal by a hybrid propulsion module
During the last 40 years, the mass of the artificial objects in orbit increased quite steadily at
the rate of about 145 metric tons annually, leading to a total tally of approximately 7000 …
the rate of about 145 metric tons annually, leading to a total tally of approximately 7000 …
Tether dynamics analysis and guidance and control design for active space-debris removal
HTK Linskens, E Mooij - Journal of Guidance, Control, and Dynamics, 2016 - arc.aiaa.org
Recent years have seen a steep increase in research being performed toward active space-
debris removal. In particular, the ESA has proposed a mission in which a robotic chaser …
debris removal. In particular, the ESA has proposed a mission in which a robotic chaser …
Survival probability of round and tape tethers against debris impact
SB Khan, JR Sanmartin - Journal of Spacecraft and Rockets, 2013 - arc.aiaa.org
The current space environment, consisting of manmade debris and micrometeoroids, poses
a risk to safe operations in space, and the situation is continuously deteriorating due to in …
a risk to safe operations in space, and the situation is continuously deteriorating due to in …
[HTML][HTML] Development status of AEOLDOS–A deorbit module for small satellites
P Harkness, M McRobb, P Lützkendorf… - Advances in Space …, 2014 - Elsevier
A prototype CubeSat module to deploy a gossamer aerobrake, using strain stored in tape-
springs, at end-of-life is described. A novel hub geometry to reduce bending shock at end-of …
springs, at end-of-life is described. A novel hub geometry to reduce bending shock at end-of …
A bare-photovoltaic tether for consumable-less and autonomous space propulsion and power generation
M Tajmar, G Sánchez-Arriaga - Acta Astronautica, 2021 - Elsevier
State-of-the-art electrodynamic tethers reach a steady electric current by using a bare
segment to capture electrons passively from the ambient plasma (anodic contact) and an …
segment to capture electrons passively from the ambient plasma (anodic contact) and an …
Performance model for space-based laser debris sweepers
M Schmitz, S Fasoulas, J Utzmann - Acta Astronautica, 2015 - Elsevier
This paper outlines the capabilities of a space-based laser for active debris removal in the
range of 1 cm to 10 cm. As for respective ground based solutions, the space based laser …
range of 1 cm to 10 cm. As for respective ground based solutions, the space based laser …
Solar radiation pressure-augmented deorbiting: passive end-of-life disposal from high-altitude orbits
A deorbiting strategy for small satellites is proposed that exploits the effect of solar radiation
pressure to increase the spacecraft orbit eccentricity so that the perigee falls below an …
pressure to increase the spacecraft orbit eccentricity so that the perigee falls below an …
Optimum sizing of bare-tape tethers for de-orbiting satellites at end of mission
JR Sanmartín, A Sánchez-Torres, SB Khan… - Advances in Space …, 2015 - Elsevier
De-orbiting satellites at end of mission would prevent generation of new space debris. A
proposed de-orbit technology involves a bare conductive tape-tether, which uses neither …
proposed de-orbit technology involves a bare conductive tape-tether, which uses neither …
Libration and transverse dynamic stability control of flexible bare electrodynamic tether systems in satellite deorbit
This paper developed a high-fidelity dynamic model of flexible space tether systems by
considering the elastic, thermal, and electrical coupling effects on the dynamics and stability …
considering the elastic, thermal, and electrical coupling effects on the dynamics and stability …