CopasAPIAutogenProgramme
Monday, April 17
14:00 - 14:30 |
Pre-Registration at ESOC Maingate Time frame: 14:00 - 17:15
Room: ESOC Maingate
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14:30 - 15:00 |
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15:00 - 15:30 |
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15:30 - 16:00 |
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16:00 - 16:30 |
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16:30 - 17:00 |
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17:00 - 17:30 |
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Tuesday, April 18
07:30 - 08:00 |
Registration Time frame: 07:30 - 09:30
Room: ESOC Gatehouse
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08:00 - 08:30 |
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08:30 - 09:00 |
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09:00 - 09:30 |
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09:30 - 10:00 |
Opening Ceremony Time frame: 09:30 - 10:40
Room: H-I/H-IV
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10:00 - 10:30 |
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10:30 - 11:00 |
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Highlight Talks Time frame: 10:40 - 12:00
Room: H-I/H-IV
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11:00 - 11:30 |
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11:30 - 12:00 |
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12:00 - 12:30 |
Opening of Exhibition Time frame: 12:00 - 12:15
Room: Press Centre
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Lunch break Time frame: 12:15 - 14:00
Room: Foyer
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12:30 - 13:00 |
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13:00 - 13:30 |
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13:30 - 14:00 |
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14:00 - 14:30 |
Radar, Optical, and in-situ Measurements - ground-based experiments Time frame: 14:00 - 16:00
Room: H-I
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Hypervelocity Impacts & Shielding: Application Time frame: 14:20 - 16:00
Room: H-IV
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14:30 - 15:00 |
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15:00 - 15:30 |
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15:30 - 16:00 |
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16:00 - 16:30 |
Coffee break Time frame: 16:00 - 16:30
Room: Foyer
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16:30 - 17:00 |
Radar, Optical, and in-situ Measurements - Space-Based Time frame: 16:30 - 18:10
Room: H-I
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Hypervelocity Impacts & Shielding: Simulations and Tests Time frame: 16:50 - 18:30
Room: H-IV
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17:00 - 17:30 |
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17:30 - 18:00 |
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18:00 - 18:30 |
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18:30 - 19:00 |
Reception Time frame: 18:30 - 20:45
Room: ESOC canteen
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19:00 - 19:30 |
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19:30 - 20:00 |
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20:00 - 20:30 |
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20:30 - 21:00 |
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Wednesday, April 19
08:00 - 08:30 |
Registration Time frame: 08:00 - 08:30
Room: Gatehouse
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08:30 - 09:00 |
Radar, Optical, and in-situ Measurements - Attitude Time frame: 08:30 - 10:30
Room: H-I
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Active Removal and Remediation: Missions and Scenarios Time frame: 08:50 - 10:50
Room: H-IV
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09:00 - 09:30 |
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09:30 - 10:00 |
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10:00 - 10:30 |
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10:30 - 11:00 |
Coffee break Time frame: 10:30 - 11:00
Room: Foyer
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11:00 - 11:30 |
Radar, Optical, and in-situ Measurements - in-situ Time frame: 11:00 - 12:40
Room: H-I
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Active Removal and Remediation: Concepts and Technologies Time frame: 11:20 - 13:00
Room: H-IV
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11:30 - 12:00 |
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12:00 - 12:30 |
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12:30 - 13:00 |
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Lunch break Time frame: 12:40 - 14:00
Room: Foyer
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13:00 - 13:30 |
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13:30 - 14:00 |
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14:00 - 14:30 |
Space Surveillance - Systems Time frame: 14:00 - 16:00
Room: H-I
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Active Removal and Remediation: Capture Techniques Time frame: 14:20 - 16:20
Room: H-IV
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14:30 - 15:00 |
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15:00 - 15:30 |
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15:30 - 16:00 |
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16:00 - 16:30 |
Coffee break Time frame: 16:00 - 16:30
Room: Foyer
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16:30 - 17:00 |
Space Surveillance - Sensor Technologies Time frame: 16:30 - 18:10
Room: H-I
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Active Removal and Remediation: Rendez-Vous and Dynamics Time frame: 16:50 - 18:30
Room: H-IV
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17:00 - 17:30 |
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17:30 - 18:00 |
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18:00 - 18:30 |
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18:30 - 19:00 |
Poster Session Time frame: 18:30 - 20:00
Room: Wintergarden
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19:00 - 19:30 |
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19:30 - 20:00 |
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20:00 - 20:30 |
Thursday, April 20
08:00 - 08:30 |
Registration Time frame: 08:00 - 08:30
Room: Gatehouse
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08:30 - 09:00 |
Space Surveillance - Astrodynamics Time frame: 08:30 - 10:30
Room: H-I
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Re-entry Risk Analysis - Tools and Techniques Time frame: 08:50 - 10:50
Room: H-IV
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09:00 - 09:30 |
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09:30 - 10:00 |
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10:00 - 10:30 |
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10:30 - 11:00 |
Coffee break Time frame: 10:30 - 11:00
Room: Foyer
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11:00 - 11:30 |
Space Surveillance - Processing and Applications Time frame: 11:00 - 12:40
Room: H-I
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Re-entry Risk Analyses - Predictions Time frame: 11:20 - 13:00
Room: H-IV
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11:30 - 12:00 |
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12:00 - 12:30 |
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12:30 - 13:00 |
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Lunch break Time frame: 12:40 - 14:00
Room: Foyer
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13:00 - 13:30 |
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13:30 - 14:00 |
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14:00 - 14:30 |
Operational Collision Avoidance Time frame: 14:00 - 16:00
Room: H-I
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Re-entry Risk Analysis - Application Time frame: 14:20 - 16:20
Room: H-IV
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14:30 - 15:00 |
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15:00 - 15:30 |
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15:30 - 16:00 |
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16:00 - 16:30 |
Coffee break Time frame: 16:00 - 16:30
Room: Foyer
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16:30 - 17:00 |
Debris & Meteoroid Environment Modeling and Prediction - Large Constellations Time frame: 16:30 - 18:10
Room: H-I
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Debris Mitigation: Techniques and Analyses Time frame: 16:50 - 18:30
Room: H-IV
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17:00 - 17:30 |
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17:30 - 18:00 |
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18:00 - 18:30 |
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18:30 - 19:00 |
Optional Conference Dinner Time frame: 18:30 - 20:45
Room: Orangerie, Darmstadt
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19:00 - 19:30 |
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19:30 - 20:00 |
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20:00 - 20:30 |
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20:30 - 21:00 |
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Friday, April 21
08:00 - 08:30 |
Registration Time frame: 08:00 - 08:30
Room: Gatehouse
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08:30 - 09:00 |
Debris & Meteoroid Environment Modeling and Prediction Time frame: 08:30 - 10:30
Room: H-I
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Debris Mitigation: Application and Processes Time frame: 08:50 - 10:50
Room: H-IV
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09:00 - 09:30 |
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09:30 - 10:00 |
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10:00 - 10:30 |
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10:30 - 11:00 |
Coffee break Time frame: 10:30 - 11:00
Room: Foyer
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11:00 - 11:30 |
Debris & Meteoroid Environment Modeling and Prediction Time frame: 11:00 - 12:40
Room: H-I
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Press Briefing with Q&A Time frame: 11:00 - 13:00
Room: H05
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Debris Mitigation: Design Solutions Time frame: 11:20 - 13:00
Room: H-IV
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11:30 - 12:00 |
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12:00 - 12:30 |
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12:30 - 13:00 |
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Lunch break Time frame: 12:40 - 14:00
Room: Foyer
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13:00 - 13:30 |
Optional technical tour Time frame: 13:00 - 17:15
Room: Technoseum Mannheim
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13:30 - 14:00 |
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14:00 - 14:30 |
Closure of conference Time frame: 14:00 - 14:15
Room: H-I
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14:30 - 15:00 |
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15:00 - 15:30 |
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15:30 - 16:00 |
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16:00 - 16:30 |
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16:30 - 17:00 |
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17:00 - 17:30 |
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Opening Ceremony
09:30 - 09:40 |
Welcome Address |
09:40 - 09:50 |
Welcome Address |
09:50 - 10:05 |
Introduction |
10:05 - 10:20 |
Space Debris Movie Premiere |
10:20 - 10:40 |
Keynote |
Highlight Talks
10:40 - 11:00 |
SENSITIVITY OF THE SPACE DEBRIS ENVIRONMENT TO LARGE CONSTELLATIONS AND SMALL SATELLITES |
11:00 - 11:20 |
Highlights of Recent Research Activities at the NASA Orbital Debris Program Office |
11:20 - 11:40 |
Current Status of Research and Development on Active Debris Removal at JAXA |
11:40 - 12:00 |
Determining and Modeling Space Debris Attitude States by Fusing Data from different Observation Techniques |
Radar, Optical, and in-situ Measurements - ground-based experiments
14:00 - 14:20 |
Use of EISCAT 3D for Observations of space debris |
14:20 - 14:40 |
Performance analysis of the large space debris tracking telescope in the North Caucasus after the second first light |
14:40 - 15:00 |
Stare and chase: Optical pointing determination, orbit calculation and satellite laser ranging within a single pass |
15:00 - 15:20 |
The Small Size Debris Population at GEO from Optical Observations |
15:20 - 15:40 |
United Kingdom Infrared Telescope’s Spectrograph Observations of Human-Made Space Objects |
15:40 - 16:00 |
Extensive light curve database of Astronomical Institute of the University of Bern |
Hypervelocity Impacts & Shielding: Application
14:20 - 14:40 |
Optimization of Debris Shields on the NISAR Mission’s L-Band Radar Instrument |
14:40 - 15:00 |
SURVEYS OF ISS RETURNED HARDWARE FOR MMOD IMPACTS |
15:00 - 15:20 |
Impact Characterization of Stuffed Whipple for China Space Station |
15:20 - 15:40 |
Investigation on solar array damage characteristic under millimeter size orbital debris hypervelocity impact |
15:40 - 16:00 |
MESO-SCALE COMPUTATIONAL MODELING OF HYPERVELOCITY IMPACT DAMAGE IN ADVANCED MATERIALS |
Radar, Optical, and in-situ Measurements - Space-Based
16:30 - 16:50 |
Preliminary concept of a space-based radar for detecting mm-size space debris |
16:50 - 17:10 |
Streak Detection and Analysis Pipeline for Space-debris Optical Images |
17:10 - 17:30 |
Optical In-Situ Monitor Breadboard System |
17:30 - 17:50 |
High efficiency robotic optical tracking of space debris from PST2 telescope in Arizona |
17:50 - 18:10 |
ASSESSMENT OF INFORMATION CONTENT CONTAINED IN OBSERVED PHOTOMETRIC SIGNATURES OF NON-RESOLVED SPACE DEBRIS OBJECTS |
Hypervelocity Impacts & Shielding: Simulations and Tests
16:50 - 17:10 |
UNDERSTANDING SPACE CRAFT FRAGMENTATION: SIMULATIONS AND EXPERIMENTS |
17:10 - 17:30 |
Characterization of Orbital Debris via Hyper-velocity Laboratory-based Tests |
17:30 - 17:50 |
Methods to Reduce Uncertainties in Spacecraft Vulnerability Predictions |
17:50 - 18:10 |
Predicting the Rupture of a Cryogenic Composite Pressure Vessel (COPV) Following a Hypervelocity Impact |
18:10 - 18:30 |
STUDY OF HYPERVELOCITY IMPACTS ON SPACE SHIELDS ABOVE 7 KM/S |
Radar, Optical, and in-situ Measurements - Attitude
08:30 - 08:50 |
Debris Attitude Motion Measurements and Modelling by Combining Different Observation Techniques |
08:50 - 09:10 |
Temporal analysis of Envisat's rotational motion |
09:10 - 09:30 |
Automated Attitude Estimation from ISAR Images |
09:30 - 09:50 |
Space debris attitude determination of faint LEO objects using photometry: SwissCube’s cubesat study case |
09:50 - 10:10 |
Determination of orbital and spin parameters of LEO satellites by Polish and Ukrainian optical observatories |
10:10 - 10:30 |
Determination of Attitude and Attitude Motion of Space Debris, using Laser Ranging and Single-Photon Light Curve Data |
Active Removal and Remediation: Missions and Scenarios
08:50 - 09:10 |
Architecture and first Achievements of a Simulation for the Approach to an uncooperative Target |
09:10 - 09:30 |
Cost analysis of active debris removal scenarios and system architectures |
09:30 - 09:50 |
The RemoveDebris ADR Mission: Preparing for an International Space Station Launch |
09:50 - 10:10 |
Choice of a suitable target for developing proposals for an ADR flight demonstration experiment |
10:10 - 10:30 |
A mission to Demonstrate the Preservation of the Geostationary Orbit |
10:30 - 10:50 |
Proposed Series of Orbital Debris Remediation Activities |
Radar, Optical, and in-situ Measurements - in-situ
11:00 - 11:20 |
Expanding Knowledge on Real Situation at High Near-Earth Orbits |
11:20 - 11:40 |
Development of the Space Debris Sensor (SDS) |
11:40 - 12:00 |
Using antennae for in-situ measurements of micrometeoroid and space debris impacts |
12:00 - 12:20 |
Environmental Estimation on Sub-millimeter-size Debris using In-situ Measurement Data |
12:20 - 12:40 |
STEP BY STEP REALIZATION OF AN OPERATIONAL ON ORBIT DETECTION NETWORK |
Active Removal and Remediation: Concepts and Technologies
11:20 - 11:40 |
e.Deorbit – ESA’s Active Debris Removal Mission |
11:40 - 12:00 |
Definition of an Automated Vehicle with Autonomous Fail-Safe Reaction Behavior to Capture and Deorbit Envisat. |
12:00 - 12:20 |
Active Debris Removal and Space Debris Mitigation using Hybrid Propulsion Solutions |
12:20 - 12:40 |
Modeling and Perspectives of Low-Work-Function Electrodynamic Tethers to Deorbit Space Debris |
12:40 - 13:00 |
IDEA OSG 1: Prelaunch Status Report |
Space Surveillance - Systems
14:00 - 14:20 |
TAROT: A network for Space Surveillance and Tracking operations |
14:20 - 14:40 |
SMARTnet – First Results of the Telescope Network |
14:40 - 15:00 |
GESTRA_Technology Aspects and Mode Design for Space Surveillance and Tracking |
15:00 - 15:20 |
Sensor Tasking for multi-sensor Space Object Surveillance |
15:20 - 15:40 |
Architectural description of the Spanish Space Surveillance and Tracking System |
15:40 - 16:00 |
Space Surveillance and Tracking in ESA's SSA programme |
Active Removal and Remediation: Capture Techniques
14:20 - 14:40 |
Orbital and Solar Storm Analysis of the Pulsed Electrostatic Tractor |
14:40 - 15:00 |
MEDUSA – Mechanism for Entrapment of Debris Using Shape memory Alloy |
15:00 - 15:20 |
Experimental setup and tests’ results for uncooperative objects capture and manoeuvring with robotic arm |
15:20 - 15:40 |
Net Capture System for Debris Removal Demonstration Mission |
15:40 - 16:00 |
Design and Testing of a Full Scale Harpoon Capture System |
16:00 - 16:20 |
Validation methods of the grippers capabilities to capture Launch Adapting Rings of the non-cooperative satellites |
Space Surveillance - Sensor Technologies
16:30 - 16:50 |
GRAVES Space Surveillance System: Life Extension and Upgrade Program |
16:50 - 17:10 |
Development of Laser Measurement to Space Debris at Shanghai SLR Station |
17:10 - 17:30 |
First Results from an ESA Study on Accurate Orbit Determination with Laser Tracking of uncooperative Targets |
17:30 - 17:50 |
Innovative Technologies for Optical Ground Stations |
17:50 - 18:10 |
Performance Assessment of the Multibeam Radar Sensor BIRALES for Space Surveillance and Tracking |
Active Removal and Remediation: Rendez-Vous and Dynamics
16:50 - 17:10 |
TETHERED-TUGS FOR ACTIVE DEBRIS REMOVAL: MICROGRAVITY EXPERIMENTAL VALIDATION OF DYNAMICS AND CONTROL |
17:10 - 17:30 |
TETHERS AS PULLING CAPTURE TECHNOLOGY FOR E.DEORBIT AND NET/HARPOON-BASED ADR MISSIONS |
17:30 - 17:50 |
Airbus DS Vision Based Navigation solutions tested on LIRIS experiment data |
17:50 - 18:10 |
An experiment of measuring position and attitude of space debris by stereo-vision in orbital optical condition |
18:10 - 18:30 |
Evaluation of Feature Detectors for Infrared Imaging in view of Active Debris Removal |
Space Surveillance - Astrodynamics
08:30 - 08:50 |
Deformation of space debris and subsequent changes in orbit during eclipse due to solar and Earth radiation fluxes. |
08:50 - 09:10 |
Fusion of laser ranges and angular measurements data for LEO and GEO space debris orbit determination |
09:10 - 09:30 |
A Novel Initial Orbit Determination Algorithm from Doppler and Angular Observations |
09:30 - 09:50 |
Automatic Domain Pruning Filter for Optical Observations on Short Arcs |
09:50 - 10:10 |
Using Conjunction Analysis Methods for Manoeuvre Detection |
10:10 - 10:30 |
Assessment of post-maneuver observation correlation using short-arc tracklets |
Re-entry Risk Analysis - Tools and Techniques
08:50 - 09:10 |
Simulation of the Ariane 5 EPC reentry with the Fragmentation tool suite |
09:10 - 09:30 |
Progress in Hybrid Spacecraft/Object Oriented Destructive Re-entry Modelling using the SAM Code |
09:30 - 09:50 |
Upgrade of DRAMA's Spacecraft Entry Survival Analysis Codes |
09:50 - 10:10 |
DEBRIS: an Object Oriented Code for Footprint, Survivability and Risk Assessment |
10:10 - 10:30 |
Uncertainty Quantification in Orbital Debris Reentry for Reliable Ground Footprint Estimation |
10:30 - 10:50 |
The definition of the Multistep Inputs Statistics method for the computation of the safety re-entry area |
Space Surveillance - Processing and Applications
11:00 - 11:20 |
Cataloguing Space objects from observations: CORTO cataloguing system |
11:20 - 11:40 |
Optical measurements association using Optimized Boundary Value IOD coupled with Markov Clustering algorithm |
11:40 - 12:00 |
Tracklet-tracklet correlation method for radar and angle observations |
12:00 - 12:20 |
Methods of Predicting and Processing Breakups of Space Objects |
12:20 - 12:40 |
ESA’s SST DATA CENTRE INTEGRATION |
Re-entry Risk Analyses - Predictions
11:20 - 11:40 |
Assessing the risk and the uncertainty affecting the uncontrolled reentry of manmade space objects |
11:40 - 12:00 |
Uncertainty Characterization of Atmospheric Density Models for Orbit Prediction of Space Debris |
12:00 - 12:20 |
Re-entry Prediction Uncertainties derived from Environmental and Observation considerations |
12:20 - 12:40 |
Thermosphere model evaluation at low altitude with GOCE densities |
12:40 - 13:00 |
Practicalities of re-entry predictions – the VEGA-01 AVUM case |
Operational Collision Avoidance
14:00 - 14:20 |
Information Theoretic Approaches to Space Object Collision |
14:20 - 14:40 |
Covariance Size and the Breakdown of Gaussianity in GEO Uncertainty Predictions |
14:40 - 15:00 |
Space Debris Braking System using derivative SRM for Just-In Time Collision Avoidance Maneuver |
15:00 - 15:20 |
Satellite collision probability for long-term encounters and arbitrary primary satellite shape. |
15:20 - 15:40 |
Current Collision Avoidance service by ESA's Space Debris Office |
15:40 - 16:00 |
GMV/ISON COMBINED OPTICAL CAMPAIGNS |
Re-entry Risk Analysis - Application
14:20 - 14:40 |
Numerical Flow Analysis of the ISS Re-Entry |
14:40 - 15:00 |
Minimum dV for Targeted Spacecraft Disposal |
15:00 - 15:20 |
Evaluation of re-entry conditions from orbits at the Lagrangian points |
15:20 - 15:40 |
On the re-entry design for the SOHO mission |
15:40 - 16:00 |
Planned yet uncontrolled re-entries of the Cluster-II spacecraft |
16:00 - 16:20 |
ESA CLEANSAT _ SMA dismantlement mechanisms |
Debris & Meteoroid Environment Modeling and Prediction - Large Constellations
16:30 - 16:50 |
A quantitative evaluation of the environmental impact of the mega constellations |
16:50 - 17:10 |
MAXIMIZING POST MISSION DISPOSAL OF MEGA CONSTELLATIONS SATELLITES REACHING END OF OPERATIONAL LIFETIME |
17:10 - 17:30 |
LUCA2 - An enhanced long-term utility for collision analysis |
17:30 - 17:50 |
Self-induced collision risk analysis for large constellations |
17:50 - 18:10 |
Optimization of constellation jettisoning regards to short term collision risks |
Debris Mitigation: Techniques and Analyses
16:50 - 17:10 |
Analysis of orbit stability in the geosynchronous region for end-of-life disposal |
17:10 - 17:30 |
MEO dynamics and GNSS disposal strategies |
17:30 - 17:50 |
Status of the Space Environment: Current Level of Adherence to the Space Debris Mitigation Policy |
17:50 - 18:10 |
SEMI-CONTROLLED REENTRY |
18:10 - 18:30 |
Tundra Disposal Orbit Study |
Debris & Meteoroid Environment Modeling and Prediction
08:30 - 08:50 |
EFFECTS OF CUBESAT DEPLOYMENTS IN LOW-EARTH ORBIT |
08:50 - 09:10 |
Risk induced by the uncatalogued space debris population in the presence of large constellations |
09:10 - 09:30 |
Assessing uncertainties in the estimation of the orbital lifetime |
09:30 - 09:50 |
Analysis of Breakup Events |
09:50 - 10:10 |
Forensic Analysis of On-Orbit Debris Generation Events |
10:10 - 10:30 |
DISCOS 3: An improved data model for ESA's Database and Information System Characterising Objects in Space |
Debris Mitigation: Application and Processes
08:50 - 09:10 |
Impacts of the Space Debris Mitigation rules on the spacecraft design in Airbus Defence and Space |
09:10 - 09:30 |
Industry Processes for Space Debris Mitigation in Early Mission Definition: Current State and Room for Improvement |
09:30 - 09:50 |
Space Debris Management of Launch Operations |
09:50 - 10:10 |
IMPACT OF SPACE DEBRIS MITIGATION REQUIREMENTS ON THE MISSION DESIGN OF ESA SPACECRAFT |
10:10 - 10:30 |
MAJOR TRENDS FOR MITIGATION OF SPACE DEBRIS IN NEAR-EARTH SPACE IN THE RUSSIAN FEDERATION |
10:30 - 10:50 |
Life Cycle Assessment Indicator for Space Debris |
Debris & Meteoroid Environment Modeling and Prediction
11:00 - 11:20 |
Extending the ECOB space debris index with fragmentation risk estimation |
11:20 - 11:40 |
IMPROVEMENT OF SPACE DEBRIS MODEL IN MEO AND GEO REGIONS ACCORDING TO THE CATALOG OF KIAM RAS |
11:40 - 12:00 |
A comparison of damaging meteoroid and orbital debris fluxes in Earth orbit |
12:00 - 12:20 |
Algorithms for the Computation of Debris Risks |
12:20 - 12:40 |
A COMPARISON OF THE SOCIT AND DEBRISAT EXPERIMENTS |
Press Briefing with Q&A
11:00 - 11:05 |
Statement |
11:05 - 11:10 |
Statement |
11:10 - 11:15 |
Statement |
11:15 - 11:20 |
Statement |
11:20 - 11:25 |
Statement |
11:25 - 11:30 |
Statement |
11:30 - 11:35 |
Statement |
11:35 - 11:40 |
Statement |
11:40 - 11:45 |
Statement |
11:45 - 13:00 |
Questions and Answers to the Panel |
Debris Mitigation: Design Solutions
11:20 - 11:40 |
Design for Demise techniques for medium/large LEO satellites reentry |
11:40 - 12:00 |
Results of the Deployable Membrane & ADEO Passive De-Orbit Subsystem Activities leading to a Dragsail Demonstrator |
12:00 - 12:20 |
Development of Commercial Drag-Augmentation Systems for Small Satellites |
12:20 - 12:40 |
ESTCube-2 plasma brake payload for effective deorbiting |
12:40 - 13:00 |
FRAGMENTATION EVENT DEBRIS FIELD EVOLUTION USING 3D VOLUMETRIC RISK ASSESSMENT |
Poster- Radar, Optical, and in-situ Measurements
18:30 - 19:12 |
Estimation of Rotating RSO Parameters using Radar Data and Joint Time-Frequency Transforms |
18:30 - 19:12 |
Photometrical Database of GSS and methods of identification satellites on their photometrical characteristics |
18:30 - 19:12 |
Light-curves of Retired Geosynchronous Satellites |
18:30 - 19:12 |
An efficient and automatic debris detection framework based on GPU technology |
18:30 - 19:12 |
Faint Streak Detection with Certificate by Adaptive Two-Level Bayesian Inference |
18:30 - 19:12 |
The ESA Space Collaborative Observation Platform (SCOOP), objectives and functionalities |
18:30 - 19:12 |
Preparing the new 2 kHz satellite laser ranging system in Finland for debris observations |
18:30 - 19:12 |
SPIN-UP OF SPACE DEBRIS CAUSED BY SOLAR RADIATION PRESSURE |
18:30 - 19:12 |
Light Curve Properties of high earth orbital rocket bodies Observed at Weihai Observatory of Shandong University |
18:30 - 19:12 |
LEDSat: Design of a CubeSat equipped with LEDs as calibration target |
18:30 - 19:12 |
Multi-band photometric observations of GEO satellites: Preliminary Results |
18:30 - 19:12 |
On-Sky Evaluation of Passive Polarimetry as a Technique to Characterise Space Debris |
18:30 - 19:12 |
Probability of Detection and Likelihood: Application to Space Object Observation |
18:30 - 19:12 |
Automatic pipeline for light-curves variability analysis of GEO objects |
18:30 - 19:12 |
Adaptive Optics for Satellite Imaging and Earth Based Space Debris Manoeuvres |
18:30 - 19:12 |
Precise orbit propagation of space debris objects using the Hermite integration scheme |
18:30 - 19:12 |
Observing Strategies for Focused Orbital Debris Surveys Using the Magellan Telescope |
18:30 - 19:12 |
GROUND-BASED OBSERVING CAMPAIGNS OF BRIZ-M DEBRIS WITH THE UKIRT AND NASA MCAT TELESCOPES |
18:30 - 19:12 |
A remote photometry telescope for space debris in Tibet |
18:30 - 19:12 |
FORTE: ISON Robotic Telescope Control Software |
18:30 - 19:12 |
The Fly-Eye Telescope Customization for Debris Discovery and Cataloguing |
Poster - Space Surveillance
18:30 - 19:12 |
Orbital Solutions to LEO-to-LEO Angles-only Very Short-arc Tracks |
18:30 - 19:12 |
Ontology for the Space Situational Awareness Programme in Europe |
18:30 - 19:12 |
The current state of the KIAM database on space debris in high orbit and its use for prediction of dangerous approaches |
18:30 - 19:12 |
Accurate Orbit Determination of Space Debris with Laser Tracking |
18:30 - 19:12 |
Determining Debris Characteristics from Observability Analysis of Artificial Near-Earth Objects |
18:30 - 19:12 |
Evaluation of Data Stream Management Systems in the Context of Space Surveillance and Tracking |
18:30 - 19:12 |
Covariance Matrix Uncertainty Analysis and Correction |
18:30 - 19:12 |
Attitude Characterization of Aerodynamic Stable Objects Based on TLE |
18:30 - 19:12 |
Accurate Optical Observations of Space Objects in GEO, and applicability to closer LEO regimes |
18:30 - 19:12 |
GENERIC DATA REDUCTION FRAMEWORK FOR SPACE SURVEILLANCE |
18:30 - 19:12 |
Assessment and Modelling of Space Surveillance Network |
18:30 - 19:12 |
Initial Orbit Determination based on the High-order Propagation of Orbit Sets |
18:30 - 19:12 |
A new tool to observe low and higher Earth orbits: the MetaTelescope |
18:30 - 19:12 |
Explained and Unexplained Momentum Impulse Transfer Events (MITEs) |
18:30 - 19:12 |
Orbit determination result with the angle-only measurement from the optical tracking network, OWL-Net |
18:30 - 19:12 |
Conceptual Design for Expert Coordination Centres Supporting Optical and Laser Observations in a SST System |
18:30 - 19:12 |
Geometric restructurization of the space object tracking problem for improved uncertainty representation |
18:30 - 19:12 |
SST Analysis tool (SSTAN) supporting Space Surveillance and Tracking (SST) services assessment |
18:30 - 19:12 |
Worldwide optical network for Space Situational Awareness |
18:30 - 19:12 |
OWL-Net : A Global network of robotic telescopes dedicated to SSA observation |
18:30 - 19:12 |
Requirements for Observation Scenarios to Maintain a Catalogue of Space Debris Objects in Geosynchronous Region |
Poster - Operational Collision Avoidance
18:30 - 18:46 |
CryoSat-2 : In-Orbit Collision Avoidance Manoeuvre Support Tools and Operation Evolutions |
18:30 - 18:46 |
Current Status of Web Services at ESA’s Space Debris Office |
18:30 - 18:46 |
Analysis of CDM Covariance Consistency in Operational Collision Avoidance |
18:30 - 18:46 |
Collision Avoidance assessment and mitigation measures for controlled GEO/GSO spacecrafts with Orbital Debris |
18:30 - 18:46 |
Determining Orbits for Collision Prediction using Dynamical Systems Theory |
18:30 - 18:46 |
POSTPROCESSED-TLE CATALOGUE FOR CONJUNCTION DETECTION WITH GEO PASSIVE OBJECTS |
18:30 - 18:46 |
Collision Risk Computation accounting for Complex geometries of involved objects |
18:30 - 18:46 |
Close Encounters of an Advanced Kind: Lessons Learned and New Approaches in Collision Risk Assessment and Mitigation |
Poster - Mitigation, Standardization, Policies, Legal Aspects
18:30 - 18:42 |
Status of the ISO Space Debris Mitigation Standards (2017) |
18:30 - 18:42 |
Accurate Flight Dynamics for ESA' Space Debris Movie: The OREKIT solution |
18:30 - 18:42 |
Long-term implications of GNSS disposal strategies for the space debris environment |
18:30 - 18:42 |
Design for Demise: Systems-level techniques to reduce re-entry casualty risk |
18:30 - 18:42 |
TeSeR – Technology for Self-Removal – First results of an H2020 Project to develop a Post-Mission-Disposal Module |
18:30 - 18:42 |
Efficient De-Orbiting of Micro- and Nano Satellites using the IFM Nano Thruster |
Poster - Debris & Meteoroid Environment Modeling and Prediction
18:30 - 19:10 |
FRAGMENTATION EVENTS ANALYSIS MAKING USE OF FRAGMENTATION EVENT MODEL AND ASSESSMENT TOOL (FREMAT) |
18:30 - 19:10 |
CARTOGRAPHIC STUDY OF THE MEO PHASE SPACE FOR PASSIVE DEBRIS REMOVAL |
18:30 - 19:10 |
Average Cross-Sectional Area of Idealized DebriSat Fragments Using Icosahedron Motivated Orientation Vectors |
18:30 - 19:10 |
A Comparison of Results from NASA's Meteoroid Engineering Model to the LDEF Cratering Record |
18:30 - 19:10 |
EFFECT OF PHASE ANGLE ON LIGHT CURVE DATA FOR FEATURE ESTIMATION OF HIGH AREA-TO-MASS RATIO SPACE OBJECTS |
18:30 - 19:10 |
GEO space debris environment determination in the earth fixed coordinate system |
18:30 - 19:10 |
A new Space Debris Environment Engineering Model SDEEM 2015 |
18:30 - 19:10 |
An Index for Ranking Active Debris Removal Targets in LEO |
18:30 - 19:10 |
Recent Extensions of the ESABASE2/Debris Impact Risk Assessment Tool |
18:30 - 19:10 |
Examination of Debris Cloud Density Resulting From Precession of Argument of Perigee Due to J2 Effect |
18:30 - 19:10 |
The contribution of NaK droplets to the space debris environment |
18:30 - 19:10 |
The study of the dynamics of mega-constellations of near-Earth space objects |
18:30 - 19:10 |
Improvements on models and analysis means for fragmentation events |
18:30 - 19:10 |
Investigation of propagation accuracy effects within the modeling of space debris |
18:30 - 19:10 |
Results of Reference Long-term Simulations Focussing on Passive Means to Reduce the Impact of Space Debris |
18:30 - 19:10 |
Meteor shower forecasting for spacecraft operations |
18:30 - 19:10 |
The impact of the increase in small satellite launch traffic on the long-term evolution of the space debris environment |
18:30 - 19:10 |
A COLLISION IN A CUBESAT CONSTELLATION |
18:30 - 19:10 |
Spatial density maps from a fragmentation |
18:30 - 19:10 |
A statistical LEO model to investigate adaptable debris control strategies |
Poster - Re-entry Risk Analyses
18:30 - 18:58 |
Space debris atmospheric entry prediction with spacecraft-oriented tools |
18:30 - 18:58 |
INFLUENCE OF OXIDATION AND EMISSIVITY FOR METALLIC ALLOYS SPACE DEBRIS DURING THEIR ATMOSPHERIC ENTRY |
18:30 - 18:58 |
Integrated Analysis System for Re-entry Risk Assessment |
18:30 - 18:58 |
High-fidelity Numerical Simulations for Destructive Re-entry of Upper Stages |
18:30 - 18:58 |
Leveraging Lessons from the Climate Change Community and the Financial Sector to Improve Space Debris Regulations |
18:30 - 18:58 |
AERO-THERMAL RE-ENTRY SENSITIVITY ANALYSIS USING DSMC AND A HIGH DIMENSIONAL MODEL REPRESENTATION-BASED APPROACH |
18:30 - 18:58 |
Calculating the Re-Entry Probability for a given Area of Interest |
18:30 - 18:58 |
Containment tether – concept study of an efficient solution to reduce the casualty area of spacecraft components |
18:30 - 18:58 |
GOCE radar-based Orbit Determination for Re-Entry Predictions and comparison with GPS-based POD |
18:30 - 18:58 |
On the demisability and survivability of modern spacecraft |
18:30 - 18:58 |
AIRBORNE OBSERVATIONS OF RE-ENTERING SPACE DEBRIS - RESULTS AND PROSPECTS |
18:30 - 18:58 |
THE APPROACH TO CASUALTY RE-ENTRY RISK MITIGATION IN COSMO-SkyMed CURRENT AND FUTURE GENERATIONS |
18:30 - 18:58 |
Two-Line Element Uncertainty for GOCE Statistical Re-entry Predictions |
18:30 - 18:58 |
ADRYANS® V5.0 – A 1-dimension object oriented survivability tool |
Poster - Debris Mitigation Techniques and Processes
18:30 - 18:50 |
Predicted lifetime of HEO space debris calculated using various atmospheric models |
18:30 - 18:50 |
How to integrate Space Debris issue into the Life Cycle Assessment of Space Missions? |
18:30 - 18:50 |
Modelling and analysis of the folding principle used in Self-deployable Deorbiting Space Structures |
18:30 - 18:50 |
Analysis of pretension and stress stiffening in Self-deployable Deorbiting Space Structures |
18:30 - 18:50 |
CleanSat - Coordinated approach reshaping technology development for space |
18:30 - 18:50 |
THE VULNERABILITY ASSESSMENT AND DEBRIS PRODUCTION RISK MITIGATION IN COSMO-SkyMed CURRENT AND FUTURE GENERATIONS |
18:30 - 18:50 |
The H2020 project ReDSHIFT: overview, first results and perspectives |
18:30 - 18:50 |
Debris Mitigation by Collision Avoidance after End-of-Mission – assessment of a disposal solution for LEO satellites |
18:30 - 18:50 |
LEO mapping for passive dynamical disposal |
18:30 - 18:50 |
Low Power Arcjet Application for End of Life Satellite Servicing |
Poster - Active Removal and Remediation Concepts
18:30 - 18:58 |
Approaches and models for flexible tether connections in active debris removal missions |
18:30 - 18:58 |
Analysis of Tumbling Space Debris Capturing Using A Tethered-Net |
18:30 - 18:58 |
SPACE DEBRIS MITIGATION AND REMEDIATION: PERSPECTIVES OF AFFORDABLE HYBRID PROPULSION IMPLEMENTATIONS |
18:30 - 18:58 |
Design of net ejector for space debris capturing |
18:30 - 18:58 |
Motion and Parameter Estimation of an Uncooperative Space Object Using Range Image Data |
18:30 - 18:58 |
Innovative Net & Space Inflatable structure for active Debris Removal (INSIDeR) |
18:30 - 18:58 |
Touchless Electrostatic Detumble of a Representative Box-and-Panel Spacecraft Configuration |
18:30 - 18:58 |
Characteristics of ablation impulse induced by repetitive laser pulse irradiations |
18:30 - 18:58 |
Radio frequency source of weakly expanding wedge-shaped xenon ion beam for contactless removal of large-sized SD objects |
18:30 - 18:58 |
Application of space tethered systems for space debris removal |
18:30 - 18:58 |
Untrackable Space Debris Active Removal Using a Nano Satellite |
18:30 - 18:58 |
Optimization of maneuvering schemes in the framework of ADR mission in LEO |
18:30 - 18:58 |
Probability of Intersection for Laser-Based Debris Removal in the Presence of Uncertainty |
18:30 - 18:58 |
Parameters design of autonomous docking module and the choice of suitable target and primary payload for ADR |
Poster - Hypervelocity Impacts & Shielding
18:30 - 18:48 |
Initial Study on Small Debris Impact Risk Assessment during Orbit Transfer to GEO for All-Electric Satellite |
18:30 - 18:48 |
A PARADIGM FOR THE DESIGN OF ORBITAL DEBRIS PROTECTION FOR SPACECRAFT COMPOSITE PRESSURE VESSELS |
18:30 - 18:48 |
Protection of Manned Spacecraft Radiator from Space Debris |
18:30 - 18:48 |
Shielding properties investigation of impact-initiated energetic materials under hypervelocity impact |
18:30 - 18:48 |
Evaluation of the hypervelocity impact resistance of FMLs by numerical simulation |
18:30 - 18:48 |
Effects of Gamma Ray Irradiation on Ejecta Size from CFRP Plates |
18:30 - 18:48 |
Fracture of Unidirectional Tensioned Polyimide Films under Simulated Space Debris Hypervelocity Impact |
18:30 - 18:48 |
Evolution of Spacecraft Orbital Motion due to Hypervelocity Impacts from Debris and Meteoroids |
18:30 - 18:48 |
DebriSat's DCS: A Database-Based Solution to the Big Data Challenges Impacting the Future Regulation of Orbital Debris |