session 5

Title

Access to Space for Small Satellite Missions

Description

A key challenge facing the viability and growth of the small satellite community is affordable and reliable space access. This is achieved through dedicated launches, ride-shares, piggyback launches, and spacecraft propulsion technologies to reach final operational orbit. Topics of interest for this session include utilization of dedicated launches, ride-share systems, auxiliary payload systems, separation and dispenser systems, and small spacecraft sub-system development that will enable efficient small satellite access to space and orbit change (e.g. propulsion systems). Includes lessons learned from users on technical and programmatic approaches. For a discussion of small launchers concepts and operations, please refer to session D2.7.

Date

2013-09-24

Time

14:45

Room

307B

IPC members
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

Long March,Easy And Reliable Access To Space For Small Satellites

accepted

15'

confirmed

Mr. Bo Liu

China Great Wall Industry Corporation (CGWIC)

China

2

LAUNCHING NANOSATS AFFORDABLY, PROBLEMS AND SOLUTIONS

accepted

15'

confirmed

Mr. Alan Webb

Commercial Space Technologies Ltd.

United Kingdom

3

Deployment system for 50+ CubeSats

accepted

15'

confirmed

Dr. Lucy Berthoud

University of Bristol

United Kingdom

4

Technical aspects of small satellites deployment from Japanese Experimental Module of ISS

accepted

15'

withdrawn

Mr. Shigeru Imai

Japan Manned Space Systems Corporation

Japan

5

Interplanetary Hitchhiking to Support Small Spacecraft Missions Beyond Earth Orbit

accepted

15'

confirmed

Mr. Donovan Torgerson

University of North Dakota

United States

6

Lessons Learned for Future Secondary Launches

accepted

15'

confirmed

Mr. Jason Andrews

United States

7

evaluation of secondary and hosted payload systems

accepted

15'

confirmed

Mr. Jonah Zimmerman

Stanford University

United States

8

RECOMMENDATIONS ON THE USE OF ELECTRIC PROPULSION FOR SMALL SATELLITES: LESSONS LEARNED FROM PROBA SATELLITES

accepted

15'

confirmed

Mr. Julien Tallineau

QinetiQ Space nv

Belgium

9

Use of piezo-motor technology in NovaSep, a separation mechanism for nano and micro satellites

accepted

15'

confirmed

Mr. Stanislaw Ostoja Starzewski

Novanano SAS

France

10

Analysis of a "Multi-customer Satellite Access" (MuSA) Approach

accepted

15'

confirmed

Mr. Simone La Torre

International Space University (ISU)

France