The dynamic similitude criteria for detachable sections of rocket like fairing leaf are presented. The criteria ensure the similarity of the center of mass and attitude motion of the small-scale model to the full scale body. The application of the presented criteria is illustrated by a numerical experiment. These criteria can be used to conduct small-scale experiment for the investigation of the re-entry motion of launch vehicles and its parts.
机构:
ESA, Estec, NL-2201 AZ Noordwijk, Netherlands
ESA, Estec, NL-2200 AG Noordwijk, NetherlandsUniv Stuttgart, IRS, Pfaffenwaldring 31, D-70569 Stuttgart, Germany
机构:
Korea Adv Inst Sci & Technol, Satellite Technol Res Ctr, Taejon 305701, South KoreaKorea Adv Inst Sci & Technol, Satellite Technol Res Ctr, Taejon 305701, South Korea
Chung, Tae-Jin
Lee, Na-Young
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机构:
KARI, Dept KOMPSAT 3 Syst Engn & Integrat, Daejeon, South KoreaKorea Adv Inst Sci & Technol, Satellite Technol Res Ctr, Taejon 305701, South Korea