| Nome |
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Effects of Passive De-Orbiting Through Drag and Solar Sails and Electrodynamic Tethers on the Space Debris Environment, file e0c31c0d-215e-4599-e053-1705fe0aef77
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493
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Life Cycle Assessment Indicator for Space Debris, file e0c31c0b-e7b6-4599-e053-1705fe0aef77
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403
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Environmental Impact of Large Constellations Through a Debris Index Analysis, file 1613d6cf-2205-4263-8223-7eaf76c85d53
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267
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Assessing the Impact of a Space Mission on the Sustainability of the Space Environment, file e0c31c11-eb1c-4599-e053-1705fe0aef77
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214
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Phase Space Description of the Debris’ Cloud Dynamics Through a Continuum Approach, file 4e098368-052e-49fe-8c7e-934d8d372661
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189
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Analysis of Possible Definitions of the Space Environment Capacity to Pursue Long-Term Sustainability of Space Activities, file e0c31c12-2266-4599-e053-1705fe0aef77
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187
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THEMIS: Tracking the Health of the Environment and Missions In Space, file 72ab36a1-65c5-4730-b20a-2ae5cccf62ab
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158
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Environmental aspects of passive de-orbiting devices, file e0c31c0d-ef1c-4599-e053-1705fe0aef77
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158
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Fragmentation model and strewn field estimation for meteoroids entry, file e0c31c11-50df-4599-e053-1705fe0aef77
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156
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e.Cube Mission: the Environmental CubeSat, file e0c31c11-0f0b-4599-e053-1705fe0aef77
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155
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Evaluation of the Share of the Space Capacity Share Used by a Mission, file acf55e99-a059-45fe-962d-05aae22d09e7
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140
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Modelling the Break-Up and Re-Entry Propagation of Meteorites Through a Continuum Approach, file e0c31c0f-bb4e-4599-e053-1705fe0aef77
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134
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A Comprehensive Ranking Framework for Active Debris Removal Missions Candidates, file e0c31c10-f96b-4599-e053-1705fe0aef77
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121
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CubeSat Mission Concept for Environmental Analysis in Low Earth Orbit, file e0c31c11-e5b7-4599-e053-1705fe0aef77
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117
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The Environmental CubeSat Mission E.Cube for Low Earth Orbit Data Acquisition, file e0c31c11-bd77-4599-e053-1705fe0aef77
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116
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Design of a Software to Assess the Impact of a Space Mission on the Space Environment, file e0c31c10-f7d9-4599-e053-1705fe0aef77
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105
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Re-entry prediction and demisability analysis for the atmospheric disposal of geosynchronous satellites, file e0c31c11-f0a2-4599-e053-1705fe0aef77
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104
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COMPASS: Control for orbit manoeuvring enhancing natural perturbations, file e0c31c0c-dd92-4599-e053-1705fe0aef77
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103
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Modeling Re-Entry Break-Up Uncertainties with Continuity Equation and Gaussian Mixture Models Interpolation, file e0c31c0f-a9ff-4599-e053-1705fe0aef77
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103
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Propagation and Reconstruction of Reentry Uncertainties Using Continuity Equation and Simplicial Interpolation, file e0c31c11-0600-4599-e053-1705fe0aef77
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99
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PUZZLE Software for the Characterisation of In-Orbit Fragmentations, file e0c31c11-5c0b-4599-e053-1705fe0aef77
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96
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A mission concept for in-orbit particle collection around asteroids, file 999528f0-47bc-416b-957a-059d6f9f943b
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94
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Spacecraft design optimisation for demise and survivability, file e0c31c0d-c780-4599-e053-1705fe0aef77
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92
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Characterising In-Orbit Fragmentations with the Puzzle Software, file e0c31c12-08cf-4599-e053-1705fe0aef77
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91
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Ejecta analysis for an asteroid impact event in the perturbed circular restricted three body problem, file e0c31c11-b05d-4599-e053-1705fe0aef77
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86
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Assessing the impact of space debris on orbital resource in life cycle assessment: A proposed method and case study, file e0c31c0c-dbd6-4599-e053-1705fe0aef77
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79
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Attitude Control of the Disposal Phase of the eCube Mission for Atmospheric Data Acquisition, file e0c31c11-54fb-4599-e053-1705fe0aef77
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78
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A Density-Based Approach to the Propagation of Re-Entry Uncertainties, file e0c31c0c-c135-4599-e053-1705fe0aef77
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76
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Interface Between the Long-Term Propagation and the Destructive Re-Entry Phases Exploiting the Overshoot Boundary, file e0c31c12-153e-4599-e053-1705fe0aef77
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74
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Demise and Survivability Criteria for Spacecraft Design Optimization, file e0c31c0f-669e-4599-e053-1705fe0aef77
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62
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Ejecta Dynamics Around Asteroids in View of In-Orbit Particle Collection Missions, file e0c31c11-eb03-4599-e053-1705fe0aef77
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55
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Sensitivity Analysis of Asteroid Ejecta Models for Future In-Orbit Sample Collection Mission, file c824d519-5644-4987-a5a5-b6af40ab41b2
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52
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Demisability and survivability sensitivity to design-for-demise techniques, file e0c31c0d-af1b-4599-e053-1705fe0aef77
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47
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Density-Based Debris Cloud Propagation and Collision Risk Estimation Through a Binning Approach, file 73872106-de6a-4fee-ad3b-f0c5add5c4d8
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41
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A Density-Based Approach to the Propagation of Re-Entry Uncertainties, file e0c31c0c-c3ae-4599-e053-1705fe0aef77
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41
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Path Planning and Control for Asteroid Ejecta Collection After a Kinetic Impact, file 3559965b-2f97-4b4c-8d4b-cdff722834c6
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40
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Ejecta models for particles generated by small kinetic impactors onto asteroid surfaces, file e0c31c11-cdb8-4599-e053-1705fe0aef77
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39
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Integrating space debris modelling to environmental impact studies thanks to the Life Cycle Assessment (LCA) framework, file e0c31c0d-11f8-4599-e053-1705fe0aef77
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38
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Target selection for Near-Earth Asteroids in-orbit sample collection missions, file 79374ba9-4d16-4dfb-b5ef-106ac003facd
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35
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Assessing the impact of Space Debris on the orbital resource in LCA, file e0c31c0c-f365-4599-e053-1705fe0aef77
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35
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Tracking the Health of the Space Debris Environment with THEMIS, file eb30f7c5-ffcb-43bf-a875-210176807e8a
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34
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Predicting the vulnerability of spacecraft components: Modelling debris impact effects through vulnerable-zones, file e0c31c0f-6faf-4599-e053-1705fe0aef77
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33
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Integrating Density-Based Uncertainty Propagation with Object-Oriented Re-Entry Models, file e0c31c11-543c-4599-e053-1705fe0aef77
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31
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Probabilistic multi-dimensional debris cloud propagation subject to non-linear dynamics, file f48b8a49-76e2-4500-88f2-a402c71332c9
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31
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In-Orbit Fragmentations Localisation: Study and Characterisation of the Events, file e0c31c12-08d0-4599-e053-1705fe0aef77
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29
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On the Demisability and Survivability of Modern Spacecraft, file e0c31c0c-235c-4599-e053-1705fe0aef77
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26
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Considering Space Debris related impacts into the LCIA Framework, file e0c31c0c-f363-4599-e053-1705fe0aef77
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26
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MSCA IF-GF, file e0c31c10-91ae-4599-e053-1705fe0aef77
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26
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Constrained optimisation of preliminary spacecraft configurations under the design-for-demise paradigm, file e0c31c10-761b-4599-e053-1705fe0aef77
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23
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Interface between the long-term propagation and the destructive re-entry phases exploiting the overshoot boundary, file e0c31c12-a387-4599-e053-1705fe0aef77
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23
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THEMIS: Tracking the Health of the Environment and Missions In Space, file 05d7de2d-a72b-4d58-92ca-ef35309de6a9
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22
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Demisability analysis of re-entering structures on resonant trajectories, file e0c31c11-47d9-4599-e053-1705fe0aef77
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19
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Comparison of continuity equation and Gaussian mixture model for long-term density propagation using semi-analytical methods, file e0c31c12-b40b-4599-e053-1705fe0aef77
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18
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Ejecta cloud distributions for the statistical analysis of impact cratering events onto asteroids’ surfaces: A sensitivity analysis, file 4ddcdfd8-be8c-4ad0-b780-9a8d8e2c3fb5
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16
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Ejecta flux estimation after an impact crater: a methodology, file 6cebb409-031f-4121-9e72-6058660d752a
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15
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A Machine Learning and Feature Engineering Approach for the Prediction of the Uncontrolled Re-Entry of Space Objects, file 879410af-7420-49a6-b908-4ea061884ec5
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11
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Interface between the long-term propagation and the destructive re-entry phases exploiting the overshoot boundary, file e0c31c12-ebdd-4599-e053-1705fe0aef77
|
10
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Spacecraft design optimisation for demise and survivability, file e0c31c0c-84c2-4599-e053-1705fe0aef77
|
9
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A mission concept for in-orbit particle collection around asteroids, file 91d34c3a-3c84-4f60-b4e3-474db1c4bb83
|
6
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Ejecta analysis for an asteroid impact event in the perturbed circular restricted three body problem, file e0c31c12-b4e0-4599-e053-1705fe0aef77
|
5
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Demisability and survivability sensitivity to design-for-demise techniques, file e0c31c0c-2482-4599-e053-1705fe0aef77
|
4
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Demisability and survivability multi-objective optimisation for preliminary spacecraft design, file e0c31c0c-78ee-4599-e053-1705fe0aef77
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4
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Demise and Survivability Criteria for Spacecraft Design Optimization, file e0c31c0d-f56a-4599-e053-1705fe0aef77
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4
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Space debris: risk and mitigation, file e0c31c0e-e184-4599-e053-1705fe0aef77
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2
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Spacecraft design optimisation for demise and survivability, file e0c31c0a-c82f-4599-e053-1705fe0aef77
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1
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Direct-drive system demonstration for a low-power hall thruster, file e0c31c0e-51f7-4599-e053-1705fe0aef77
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1
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Space Debris Cloud Propagation Through Phase Space Domain Binning, file e0c31c11-f596-4599-e053-1705fe0aef77
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1
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| Totale |
5.203 |