Identifying the 50 statistically-most-concerning derelict objects in LEO

D McKnight, R Witner, F Letizia, S Lemmens… - Acta Astronautica, 2021 - Elsevier
This paper describes a process for identifying the intact objects in orbit that (a) pose the
greatest debris-generating potential risk to operational satellites or (b) would reduce the risk …

Review of path planning in prospective multi-target active debris removal missions in low earth orbits

AA Baranov, DA Grishko - Progress in Aerospace Sciences, 2024 - Elsevier
Trends in space technology development and rapidly increasing traffic in outer space are
likely to lead to the emergence of a market for services for the removal of large debris …

Analysis of the space debris objects nozzle capture dynamic processed by a telescopic robotic arm

VI Mayorova, GA Shcheglov, MV Stognii - Acta Astronautica, 2021 - Elsevier
The paper considers a new layout of a two-stage spacecraft designed to remove a group of
large space debris objects such as the upper stages of 'Zenit'launch vehicles from low-earth …

[PDF][PDF] Разработка методов расчета параметров маневров космических аппаратов в окрестностях круговой орбиты

АА Баранов - 2019 - keldysh.ru
Важное место в процессе полета большинства космических аппаратов (КА) занимают
его манёвры–целенаправленное изменение параметров орбиты КА с помощью …

Feasibility analysis of LEO and GEO large space debris de/re-orbiting taking into account launch mass of spacecraft-collector and its configuration layout

AA Baranov, DA Grishko, GA Shcheglov… - Advances in Space …, 2021 - Elsevier
Abstract Analysis of the efficiency of two basic strategies for de/re-orbiting large space debris
objects to disposal orbits (DO) is given. Large objects in LEO are classified into groups with …

Altitude optimality boundary of two variants of large space debris removal to disposal orbits

DA Grishko, AA Baranov, GA Shcheglov - Acta Astronautica, 2024 - Elsevier
The article considers the mission design problem for removal of large space debris objects
from near-Earth orbits. It is assumed that a single active spacecraft-collector (SC) should …

Optimal transfer schemes between space debris objects in geostationary orbit

AA Baranov, DA Grishko, ОI Khukhrina, D Chen - Acta astronautica, 2020 - Elsevier
The paper compares two variants of re-orbiting space debris objects from the
geosynchronous (GEO) region. Under the first re-orbiting variant, a spacecraft-collector …

Application of additional inflatable aerodynamic device to ensure the required degradation of the disposal orbit of large-size space debris

GA Shcheglov, AA Baranov, DA Grishko… - Advances in Space …, 2023 - Elsevier
The paper studies the effectiveness of joint application of active and passive space debris
removal technologies in low-Earth orbits. An active spacecraft-collector (SC), equipped with …

Flyby of large-size space debris objects and their transition to the disposal orbits in LEO

AA Baranov, DA Grishko, YN Razoumny… - Advances in Space …, 2017 - Elsevier
The article focuses on the flyby issue involving large-size space debris (LSSD) objects in
low Earth orbits. The data on overall sizes of the known upper-stages and last stages of …

[PDF][PDF] Spacecrafts service operations as a solution for space debris problem

V Zelentsov, G Shcheglov, V Mayorova… - International Journal of …, 2018 - researchgate.net
An automatic spacecraft (SC) is probably the only type of an involved engineering device
that is currently devoid of a full system for technical maintenance and repair. When changing …