Deployable techniques for small satellites
Y Miyazaki - Proceedings of the IEEE, 2018 - ieeexplore.ieee.org
A deployable structure serves an important function in small satellites as their performance
is improved steadily. Larger deployable solar array paddles are expected as the satellite …
is improved steadily. Larger deployable solar array paddles are expected as the satellite …
Self-deployable drag sail folded nine times
JÁ Nikolajsen, AS Kristensen - Advances in Space Research, 2021 - Elsevier
Increased focus on space debris push regulations by the UN and thereby the demand for
debris removal systems to be implemented in future spacecraft. This research focuses on …
debris removal systems to be implemented in future spacecraft. This research focuses on …
Influence of satellite motion control system parameters on performance of space debris capturing
M Akhloumadi, D Ivanov - Aerospace, 2020 - mdpi.com
Relative motion control problem for capturing the tumbling space debris object is
considered. Onboard thrusters and reaction wheels are used as actuators. The nonlinear …
considered. Onboard thrusters and reaction wheels are used as actuators. The nonlinear …
TeSeR–Technology for Self-Removal–Status of a Horizon 2020 project to ensure the Post-Mission-Disposal of any future spacecraft
P Voigt, C Vogt, R Schubert… - … of the 69th …, 2018 - openresearch.surrey.ac.uk
One major source of new space debris are spacecraft (S/C) that are not removed from orbit
after the end of their operational lifetime. Many regulations (eg ISO 24113) require the …
after the end of their operational lifetime. Many regulations (eg ISO 24113) require the …
Modelling and Analysis of the Folding Principle used in Selv-Deployable Deorbiting Space Structures
JÁ Nikolajsen, PR Lauridsen… - The 7th European …, 2017 - vbn.aau.dk
An initial prototype of the Self-deployable Deorbiting Space Structure (SDSS) for semi-
controlled debris removal was launched in 2014. The SDSS module consists of 3 main …
controlled debris removal was launched in 2014. The SDSS module consists of 3 main …
Analysis of pretension and stress stiffening in a self-deployable deorbiting space structure
PR Lauridsen, JÁ Nikolajsen… - The 7th European …, 2017 - vbn.aau.dk
In the development of the Self-deployable Deorbiting Space Structure (SDSS)[1][2] FEA are
used to determine the stress state during the folding process of a given rectangular Highly …
used to determine the stress state during the folding process of a given rectangular Highly …
[PDF][PDF] Modelling of Structural Loads in Drag Augmented Space Debris Removal Concepts
AS KRISTENSEN, J NIKOLAJSEN, PR LAURIDSEN - NSCM 30, 2017 - core.ac.uk
A Self-deployable Deorbiting Space Structure (SDSS) is used for drag augmented space
debris removal. A highly flexible frame allows for a folding of the structure by bifurcation. This …
debris removal. A highly flexible frame allows for a folding of the structure by bifurcation. This …
[PDF][PDF] TeSeR–Technology for Self-Removal–Status of a Horizon 2020 project to ensure the Post-Mission-Disposal of any future spacecraft Philipp Voigta*, Cornelius …
K Konstantinidisf, M Vallig, S Brillig, T Lipsh, LL Pérezi… - 2018 - athene-forschung.unibw.de
One major source of new space debris are spacecraft (S/C) that are not removed from orbit
after the end of their operational lifetime. Many regulations (eg ISO 24113) require the …
after the end of their operational lifetime. Many regulations (eg ISO 24113) require the …