session 2

Title

Modelling and Risk Analysis

Description

This session will address the characterization of the current and future debris population and methods for in-orbit and on-ground assessments. The in-orbit analysis will cover collission risk estimates based on statistical population models and deterministic catalogues, and active avoidance.

Date

2014-09-30

Time

09:45

Room

801B

IPC members
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

Massive Collisions in LEO - A Catalyst to Initiate ADR

accepted

18'

confirmed

Dr. Darren McKnight

Integrity Applications Incorporated (IAI)

United States

2

discussion on the necessity of orbital debris removal in the geostationary region

accepted

18'

confirmed

Mr. Satoshi Furuta

Kyushu University

Japan

3

sensitivity analysis of the long term evolution of space debris population in leo

accepted

18'

confirmed

Mr. Juan Carlos Dolado Perez

Centre National d'Etudes Spatiales (CNES)

France

4

The effect of modelling assumptions on predictions of the space debris environment

accepted

18'

confirmed

Mr. Richard Blake

University of Southampton

United Kingdom

5

Influence of solar activity on long term propagations

accepted

18'

confirmed

Mr. Benjamin Bastida Virgili

European Space Agency (ESA)

Germany

6

Deriving the spacecraft environment criticality from Monte-Carlo simulations of the space debris environment

accepted

18'

confirmed

Mr. Jonas Radtke

Technische Universität Braunschweig

Germany

7

Evaluation index for the ranking of LEO objects

accepted

18'

confirmed

Dr. Elisa Maria Alessi

IFAC-CNR

Italy

8

ORDEM 3.0 and MASTER-2009 modeled small debris population comparison

accepted

18'

confirmed

Dr. Paula H. Krisko

National Aeronautics and Space Administration (NASA)

United States

9

ORDEM 3.0 and the Risk of High-Density Debris

accepted

18'

withdrawn

Dr. Mark Matney

National Aeronautics and Space Administration (NASA), Johnson Space Center

United States

10

Hypervelocity Impact Testing of DebriSat to Improve Satellite Breakup Modeling

accepted

18'

confirmed

Mr. Moises Rivero

University of Florida

United States