다단 고체연료 우주발사체의 비행궤적 해석 : 궤적 최적화와 유도Flight trajectory analysis of multi-staged launcher using solid propellant : trajectory optimization and guidance
- Advisors
- 탁민제researcher; Tahk, Min-Jearesearcher
- Description
- 한국과학기술원 : 항공우주공학과,
- Publisher
- 한국과학기술원
- Issue Date
- 1992
- Identifier
- 59946/325007 / 000901546
- Language
- kor
- Description
학위논문(석사) - 한국과학기술원 : 항공우주공학과, 1992.2, [ [iii], 44 p. ]
- Appears in Collection
- AE-Theses_Master(석사논문)
- Files in This Item
- There are no files associated with this item.
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