session 4

Title

Mitigation and Standards

Description

This session will focus on the definition and implementation of debris prevention and reduction measures and vehicle passive protection. The session will also address space debris mitigation guidelines and standards that exist already or are in preparation at the national or international level.

Date

2014-09-30

Time

14:45

Room

801B

IPC members
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

An Assessment of CubeSat Collision Risk

accepted

18'

confirmed

Dr. Hugh G. Lewis

University of Southampton

United Kingdom

2

A compact storage deorbiting sail for cubesat applications

accepted

18'

confirmed

Mr. Marcello Valdatta

Alma Mater Studiorum - University of Bologna

Italy

3

Generic Model for the Space Debris Mitigation Analysis Procedure of Cubesats

accepted

18'

confirmed

Mr. Pouyan Azari

University of Würzburg

Germany

4

analysis of mitigation guidelines compliance at International level in low earth orbit

accepted

18'

confirmed

Mr. Juan Carlos Dolado Perez

Centre National d'Etudes Spatiales (CNES)

France

5

Compliance of the Italian satellites in low Earth orbit with the end-of-life disposal guidelines for space debris mitigation

accepted

18'

confirmed

Dr. Luciano Anselmo

ISTI-CNR

Italy

6

New Insights into the Stability of the Space Debris Environment

accepted

18'

confirmed

Dr. David Finkleman

SkySentry, LLC

United States

7

Debris Creation in Geostationary Transfer Orbits: A Review of Launch Practices 2004-2012

accepted

18'

confirmed

Mr. Scott Fisher

Space Generation Advisory Council (SGAC)

United Kingdom

8

Domains of Application for Debris Mitigation Technologies

accepted

18'

withdrawn

Mr. Andrew Wolahan

ESTEC, European Space Agency

The Netherlands

9

Towards the Generalisation of Thermal Flux Data for the Improvement of Atmospheric Entry and Spacecraft Deorbiting Simulations

accepted

18'

confirmed

Mr. Nathan Donaldson

University of Oxford

United Kingdom

10

the passivation process for cryogenic stage of LM-3A launch vehicle

accepted

18'

withdrawn

Mr. Wei Hu

China Academy of Launch Vehicle Technology(CALT)

China