发明名称 Filling device for cryogenic rocket fuel, automatically separated at launching.
摘要 <p>To carry out the filling of the cryogenic propulsion units of a launcher with fuel up to the moment of the launching of the latter, there is provided a device comprising a tube portion (20) connecting the pipelines to the ground and mounted on board the launcher (12). An embrittled zone (22) of this tube portion is broken automatically during launching by means of a mechanism (24, 38) exerting a pull on the portion. This mechanism comprises a plurality of assemblies of links (26, 28) bearing on the tube portion on either side of the embrittled zone, and a bearing surface (38a, 38b) formed in a sleeve (38) which is fixed relative to the ground and with which a protuberance (26a), formed on one of the links of each assembly (26, 28), is in contact. …<IMAGE>… </p>
申请公布号 EP0371867(B1) 申请公布日期 1993.11.03
申请号 EP19890403276 申请日期 1989.11.27
申请人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE 发明人 LANDAT, JACQUES
分类号 F41A9/00;B64G1/40;B64G1/64;B64G5/00;F02K9/44;F16L55/10;F17C9/00;F41F3/055;F42B15/00;(IPC1-7):B64G1/40 主分类号 F41A9/00
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