发明名称 |
DEVICE FOR SEPARATION OF BALLISTIC MISSILE SECTION |
摘要 |
FIELD: rocket manufacturing. SUBSTANCE: the device uses a self-contained powder rocket engine and a mechanism for elimination of rigid coupling between the section and missile located in the section body. The engine nozzle is oriented relative to the section outside in radial direction at an angle to the section longitudinal axis determined from relationship: <EMI ID=0.35 HE=6 WI=42 TI=CHI>, where: r-section radius, m-section mass, J-section rolling moment, L-distance between the point of intersection of the nozzle longitudinal axis with the section outer surface and the projection of the center of masses onto the external generator of its surface. EFFECT: reduced mass and overall dimensions. 1 dwg
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申请公布号 |
RU2128816(C1) |
申请公布日期 |
1999.04.10 |
申请号 |
RU19940030025 |
申请日期 |
1994.08.09 |
申请人 |
GOSUDARSTVENNYJ RAKETNYJ TSENTR "KB. IM. AKADEMIKA;V P MAKEEVA |
发明人 |
BORZOV V.S.;KAMALEEV R.Z.;MARUSIK A.F. |
分类号 |
F42B15/36;(IPC1-7):F42B15/36 |
主分类号 |
F42B15/36 |
代理机构 |
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主权项 |
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地址 |
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