发明名称 COUPLING/DECOUPLING DEVICE FOR BOOSTER ROCKET AND ROCKET
摘要 PROBLEM TO BE SOLVED: To reduce decoupling shock, and securely achieve decoupling in a coupling/decoupling device for a booster rocket from a rocket. SOLUTION: A thrust strut 10 for coupling the booster rocket to a rocket body is composed of cases 1 and 2 connected to each other by screw parts 3, and the case 1 has thickness t11 and t12, where t11>t12. The case 2 has thickness t21 and t22, where t21>t22. A holder 43 is engaged with the outer circumference of the case 2 on the outer side, a groove 44 is provided along the whole circumference of the holder 43, and molded explosive 46 is inserted into the groove 44. The cases 1 and 2 face the groove 44 at their thin parts, and compression load is received by the case 1 and an abutment part 5, while tensile load is received by the case 2. Since the tensile load is small, the thickness t22 of the thin part of the case 2 can be thinner. By explosion of the explosive 46, the thin part is ruptured, thereby decoupling shock can be reduced.
申请公布号 JP2002211500(A) 申请公布日期 2002.07.31
申请号 JP20010005397 申请日期 2001.01.12
申请人 MITSUBISHI HEAVY IND LTD 发明人 KOBAYASHI MITSURU
分类号 B64G1/64;B64G1/00;(IPC1-7):B64G1/64 主分类号 B64G1/64
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