DESIGN AND PERFORMANCE EVALUATION OF LAB-SCALE HYBRID THRUSTER USING CATALYTICALLY DECOMPOSED HYDROGEN PEROXIDE
- Publisher
- International Aeronautical Congress
- Issue Date
- 2013-09-25
- Language
- ENG
- Citation
64th International Aeronautical Congress
- Appears in Collection
- AE-Conference Papers(학술회의논문)
- Files in This Item
- There are no files associated with this item.
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