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1.发明公开SPACECRAFT, METHOD FOR BUILDING SUCH A SPACECRAFT, AND ADAPTOR TO BE USED IN SUCH A SPACECRAFT 有权飞船，方法建设这样的航天器这类空间车辆的情况下使用SANTANDER ADAPTER
公开(公告)号：EP1492706A1
公开(公告)日：2005-01-05
申请号：EP03745477.4
申请日：2003-03-26
申请人： Dutch Space B.V.
摘要： The invention relates to a method of assembling a spacecraft (1), comprising a carrier rocket (2) and at least a first payload (3), such as a satellite or the like, wherein the first payload is placed on the carrier rocket employing an adapter (4) between the carrier rocket and the first payload, wherein a two-part adapter is used, wherein a first relatively light part (5) of the adapter is mounted under the first payload, and a second relatively heavy part (6) of the adapter is placed on the carrier rocket, after which the first part of the adapter together with the first payload is placed on the second part of the adapter and the first part of the adapter is secured is a permanent connection on the second part of the adapter so as to bring the same into the completed form.
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2.发明授权SPACECRAFT, METHOD FOR BUILDING SUCH A SPACECRAFT, AND ADAPTOR TO BE USED IN SUCH A SPACECRAFT 有权太空飞行器，建造这种太空飞行器的方法，以及用于这种太空飞行器的适配器
公开(公告)号：EP1492706B1
公开(公告)日：2005-08-31
申请号：EP03745477.4
申请日：2003-03-26
申请人： Dutch Space B.V.
摘要： The invention relates to a method of assembling a spacecraft (1), comprising a carrier rocket (2) and at least a first payload (3), such as a satellite or the like, wherein the first payload is placed on the carrier rocket employing an adapter (4) between the carrier rocket and the first payload, wherein a two-part adapter is used, wherein a first relatively light part (5) of the adapter is mounted under the first payload, and a second relatively heavy part (6) of the adapter is placed on the carrier rocket, after which the first part of the adapter together with the first payload is placed on the second part of the adapter and the first part of the adapter is secured is a permanent connection on the second part of the adapter so as to bring the same into the completed form.
摘要翻译： 本发明涉及一种组装航天器（1）的方法，该航天器包括运载火箭（2）和至少第一有效载荷（3），诸如卫星等，其中第一有效载荷被放置在运载火箭上 在所述运载火箭和所述第一有效载荷之间的适配器（4），其中使用两部分适配器，其中所述适配器的第一较轻部分（5）安装在所述第一有效载荷下方，以及相对较重的第二部分 ）放置在载体火箭上，之后将适配器的第一部分与第一有效载荷一起放置在适配器的第二部分上，并且将适配器的第一部分固定为第二部分上的永久连接 的适配器，以便将其带入完整的表格。
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