session 6
New Missions Enabled by New Propulsion Technology and Systems
- type
oral
- Description
The session will explore concepts for new missions that can be enabled by specific advancements in propulsion and/or integration of various propulsion technologies and systems.
- Date
2017-09-28
- Time
- Room
- IPC members
Co-Chair: Mr. Giorgio Saccoccia, European Space Agency (ESA), France;
Co-Chair: Dr. Jerrol Littles, Aerojet Rocketdyne, United States;
Rapporteur: Mrs. Elena Toson, Space Generation Advisory Council (SGAC), Italy;
Rapporteur: Dr. Alexander Lovtsov, SSC Keldysh Research Centre, Russian Federation;
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
---|---|---|---|---|---|---|---|
1 | 14:45 | 15 | withdrawn | Mr. Hugh Carrigg | Australia | ||
2 | 15:00 | Application for Spacecraft in Very Low Orbits Based on Air-Breathing Electric Propulsion System | 15 | no-show | Mr. xiaoye wang | Lanzhou Institute of Physics, China Academy of Space technology | China |
3 | 15:15 | 15 | confirmed | Mr. Didier Maxence | Delft University of Technology (TU Delft) | The Netherlands | |
4 | 15:30 | 15 | confirmed | Prof. Jianguo Huang | Beijing Institute of Spacecraft Environment Engineering | China | |
5 | 15:45 | 15 | confirmed | Mr. Francesco Romano | Institute of Space Systems, University of Stuttgart | Germany | |
6 | 16:00 | Feasibility of an Integrated Solar Thermal Power and Propulsion System for Small Satellites | 15 | confirmed | Ms. Fiona Leverone | Delft University of Technology (TU Delft), The Netherlands | The Netherlands |
7 | 16:15 | 15 | confirmed | Ms. Martina Mammarella | Politecnico di Torino | Italy | |
8 | 16:30 | Stationkeeping with an electrospray propulsion system for low lunar polar mission on a 6U CubeSat | 15 | confirmed | Mr. Michele Benetti | Politecnico di Milano | Italy |
9 | 16:45 | Unique Advantages of Hybrid Rocket Technology for Mars Missions | 15 | no-show | Prof.Dr. arif karabeyoglu | Koc University | United States |
10 | 17:00 | Finding NewSpace: Mission Scenarios Utilizing LOTUS: Lander/Orbiter Trans-Upper Stage | 15 | confirmed | Mr. Chrishma Singh-Derewa | National Aeronautics and Space Administration (NASA), Jet Propulsion Laboratory | United States |
11 | 17:15 | Overview and Analysis of Msail and Esail Propulsion for Interplanetary Misions | 15 | confirmed | Prof. Harijono Djojodihardjo | Indonesia | |
12 | 17:30 | Increasing the Accuracy of Electric Sail Mission Performance Estimates | 15 | confirmed | Mr. Thomas Gemmer | North Carolina State University | United States |