session 1
- Title
Space Structures I - Development and Verification (Space Vehicles and Components)
- type
oral
- Description
The topics to be addressed include evaluation of analysis versus test results, spacecraft and launch vehicles system and subsystems e.g. pressurized structures, tanks, loads introduction, primary structures, fluidic equipment, control surfaces; examination of both on-ground and in-orbit testing, launch dynamic environment as related to structural design, space vehicles development and launch verification such as sine, random and acoustic vibration testing, and lessons learned.
- Date
2009-10-12
- Time
- Room
- IPC members
Chairman: Mr. Alwin Eisenmann, IABG Industrieanlagen - Betriebsgesellschaft mbH, Germany;
Chairman: Dr. Andreas Rittweger, DLR (German Aerospace Center), Germany;
Rapporteur: Mr. Jean-Alain Massoni, Thales Alenia Space France, France;
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
---|---|---|---|---|---|---|---|
1 | Turbopump Rotordynamic Analysis for a 75ton Class Liquid Rocket Engine | 15' | Dr. Seong Min Jeon | Korea Aerospace Research Institute (KARI) | Korea, Republic of | ||
2 | Development of Combustion Chamber Nozzle by Superplastic Blow Forming with Diffusion Bonding | 15' | Dr. Yeong-Moo Yi | Korea Aerospace Research Institute (KARI) | Korea, Republic of | ||
3 | structural design of combustion chamber nozzle for a bulging process | 15' | Dr. Chul-Sung Ryu | Korea Aerospace Research Institute (KARI) | Korea, Republic of | ||
4 | Thermal Characteristics for KSLV-1 Kick Motor Nozzle on Ground Firing Test | 15' | Dr. Jae-Seok Yoo | Korea Aerospace Research Institute (KARI) | Korea, Republic of | ||
7 | Analysis and Improved Design of Structural Dynamics for the Advanced Upper Stage | 15' | Mr. Weifeng Hu | China Academy of Launch Vehicle Technology (CALT) | China | ||
8 | Satellite Simulator Development for Ground Test of Launch Vehicle | 15' | Mr. Sun-Won Kim | Korea Aerospace Research Institute (KARI) | Korea, Republic of | ||
9 | Exponential Cyclic Testing – a New Method of Assessing Flight Structures | 15' | Mr. Ian Bryce | Australian Space Research Institute | Australia | ||
10 | 15' | Mr. Yukitomo Nagao | Mitsubishi Heavy Industries, Ltd. | Japan | |||
11 | design-oriented structural analysis of filament wound shells using equivalent plate methodology | 15' | Dr. Fei Yan | Shanghai Institute of Space Propulsion | China | ||
12 | Research on the random vibration specification based on the hybrid FE-SEA method | 15' | Dr. Yuanjie Zou | China Academy of Space Technology (CAST) | China |