원문정보
초록
영어
In this study, the structural integrity of the composite rocket motor case of a space launch vehicle was evaluated by conducting compression and bending tests. Two composite rocket motor case specimens with different stacking patterns were prepared for each test, and a dedicated jig was designed and manufactured. The test procedure was developed and applied separately for compression and bending tests. By performing these tests, the composite rocket motor case structural safety was assessed.
목차
ABSTRACT
1. 서론
2. 복합재 압력용기 시험절차
2.1 복합재 압력용기 압축시험
2.2 복합재 압력용기 굽힘시험
3. 시험결과
3.1 복합재 압력용기 압축시험
3.2 복합재 압력용기 굽힘시험
4. 결론
References
1. 서론
2. 복합재 압력용기 시험절차
2.1 복합재 압력용기 압축시험
2.2 복합재 압력용기 굽힘시험
3. 시험결과
3.1 복합재 압력용기 압축시험
3.2 복합재 압력용기 굽힘시험
4. 결론
References
키워드
저자정보
참고문헌
자료제공 : 네이버학술정보