发明名称 PENETRATOR FOR STUDY OF CELESTIAL BODY SURFACES
摘要 FIELD: space engineering. SUBSTANCE: penetrator includes nose section penetrated in soil and tail section remaining on surface; both sections have compartments where experimental and working equipment items are arranged; items of equipment are interconnected by means of cables. Tail section deceleration member is made in the form of pressure chamber located between separable members of penetrator. Tail section is provided with ferrule for mounting the instrument bay and aerodynamic surface made in the form of truncated cone whose lesser base is connected with this ferrule. Instrument bay and nose section of penetrator are located in ferrule of tail section for axial displacement cavity between them where piston engageable with nose member is mounted. This cavity is brought in communication with gas reservoir by means of passage available in ferrule which provided with instrument bay and piston travel limiter. EFFECT: enhanced reliability of penetrator due to low center of mass. 2 dwgt
申请公布号 RU2111900(C1) 申请公布日期 1998.05.27
申请号 SU19914538462 申请日期 1991.01.10
申请人 NAUCHNO-PROIZVODSTVENNOE OB"EDINENIE IM.S.A.LAVOCH;N PROIZV OB EDINENIE IM S A LA 发明人 AKULOV JU.P.;AKULOV JU.P.
分类号 B64G1/00;B64G1/10;B64G1/62;(IPC1-7):B64G1/00 主分类号 B64G1/00
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