session 1
- Title
Propulsion Systems I
- Description
This session is dedicated to all aspects of Liquid rocket Engines.
- Date
2008-09-29
- Time
- Room
- IPC members
Chairman: Mr. Masahiro Atsumi, Mitsubishi Heavy Industries, Ltd., Japan;
Chairman: Mr. Max Calabro, The Inner Arch, France;
Rapporteur: Mr. Walter Zinner, ArianeGroup, Germany;
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
|---|---|---|---|---|---|---|---|
1 | presentation | Mr. Harry A. Cikanek | National Oceanic and Atmospheric Administration (NOAA) | United States | |||
2 | Liquid Oxygen/Liquid Methane Ascent Main Engine Technology Development | presentation | Mr. Joel W. Robinson | National Aeronautics and Space Administration (NASA), Marshall Space Flight Center | United States | ||
3 | The main engine of first stage of "Angara" launch-vehicles family | presentation | Dr. Igor Fatuev | NPO Energomash | Russian Federation | ||
4 | Main engine for Vega launch vehicle stage IV Results of experimental testing and qualification | presentation | Dr. Vladimir Shnyakin | Yuzhnoye State Design Office | Ukraine | ||
5 | structural analysis of propulsion system components of an indigenous cryogenic rocket engine | presentation | Mr. A.K. Asraff | Indian Space Research Organization (ISRO) | India | ||
6 | an experimental design verification of the dual-bell nozzles | presentation | Dr. yibai wang | Beijing University of Aeronautics and Astronautics (BUAA) | China | ||
7 | presentation | Mr. Eric Veith | Aerojet Rocketdyne | United States | |||
8 | discussion | Mr. Hiroyuki Kobayashi | Mitsubishi Heavy Industries, Ltd. | Japan | |||
9 | discussion | Mr. Philippe James | Safran Aircraft Engines | France | |||
10 | optimizing the quantity of propellant in nigcomsat-1 satellite using thermal knocking technique | discussion | Mr. Michael Kio | National Space Research and Development Agency (NASRDA) | United Kingdom | ||
11 | discussion | Ms. min xiang | China |