2. Modelling and Risk Analysis

Papers

1. A “Worn-out Net” Model for Analysis of Conflicts in a Multitude of Orbital Objects

2. estimation of orbital environment incorporating environmental change due to major breakups utilizing in-situ measurements

3. Demisability of critical spacecraft components during atmospheric re-entry

4. Development of new analytical models for pressure and heat flux distribution on space debris afterbodies

5. Improved representation of destructive spacecraft re-entry from analysis of high enthalpy wind tunnel tests of spacecraft structures and equipment

6. Particle flux analysis with the updated MASTER model

7. GEO and MEO Space Debris Model Improvement Based on the Catalog of KIAM RAS

8. Expected collision avoidance manoeuvre rates in DRAMA-ARES based on a history of Conjunction Data Messages

9. Assessing Potential for Cross-Contaminating Breakup Events from LEO to GEO

10. Effects of passive de-orbiting through drag and solar sails and electrodynamic tethers on the space debris environment

11. Examination of DebriSat Fragment Characteristics for Improved Fragmentation Modeling

12. Use of an Optimisation Technique for the Correlation of Aerodynamic Data on Geometric Primitives for Debris Demise Calculations