session 3
- Title
Upper Stages, Space Transfer, Entry and Landing Systems
- Description
Discussion of existing, planned or new advanced concepts for cargo and human orbital transfer. Includes current and near term transfer, entry and landing systems, sub-systems and technologies for accommodating crew and cargo transfer in space.
- Date
2013-09-24
- Time
- Room
- IPC members
Chairman: Mr. Shayne Swint, National Aeronautics and Space Administration (NASA), Marshall Space Flight Center, United States;
Chairman: Dr. Oliver Kunz, Beyond Gravity, Switzerland;
Rapporteur: Dr. Gennaro Russo, Campania Aerospace District, DAC, Italy;
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
|---|---|---|---|---|---|---|---|
1 | Aerothermodynamic and TPS Design Analysis of the USV3 Re-Entry Vehicle | 15' | confirmed | Dr. Davide Cinquegrana | CIRA Italian Aerospace Research Centre | Italy | |
2 | 15' | Mr. Johann HENOCQUE | Airbus DS GmbH | Germany | |||
3 | Mission Concept and Technical Subjects of HTV-R (HTV-Return) | 15' | withdrawn | Mr. Yusuke Suzuki | Japan Aerospace Exploration Agency (JAXA) | Japan | |
4 | CARAVAN Cargo Autonomous Rendezvous And Velocity Adjustment/Navigation | 15' | confirmed | Mr. Udrivolf Pica | International Space University (ISU) | Russian Federation | |
5 | A Study of Reentry Blackout Alleviation Using Electron Bunching in the Reentry Plasma Layer | 15' | withdrawn | Mr. Siddharth Krishnamoorthy | Student | United States | |
6 | Applied Magneto-aerodynamics for safer re-entry of space vehicle. | 15' | confirmed | Mr. Aakash Chhunchha | SRM University, Chennai | India | |
7 | 15' | withdrawn | Mr. Balbir Singh | Manipal Institute of Technology, Manipal University | India | ||
8 | Modeling and Analyzing of the Soft-landing Phase of Parachute-Retrorocket System | 15' | confirmed | Mr. Huang Wei | Beijing Institute of Mechanical & Electrical Engineering | China | |
9 | 15' | confirmed | Dr. Jingqi Cai | China Academy of Launch Vehicle Technology (CALT) | China | ||
10 | Design philosophy for OTV operating on cryogenic propellant components | 15' | Mr. Dmitry Loupiak | Energia RSC | Russian Federation | ||
11 | Space Launch System Evolvability Assessment: Upper Stage Definition | 15' | Mr. Jon Holladay | NASA | United States |