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Releasable payload shell for connecting a payload fairing, a payload and a payload propulsion unit

机译:可释放的有效载荷外壳,用于连接有效载荷整流罩,有效载荷和有效载荷推进单元

摘要

A payload section (14) of a rocket, having a payload fairing (16) and a center section (18), which comprises a payload (20) and a payload propulsion unit (22) arranged behind the payload (20) and connected with the payload (20). For preventing, or respectively limiting, a mutual relative movement, the payload fairing (16) and the center section (18) are connected by means of a connection arrangement, which is attached to the payload fairing (16) and also releasably to the center section (18). The connection arrangement is embodied as a preferably flat shell (24), which can consist of two partial shells (24.1, 24.2), which are releasably fastened to each other.
机译:火箭的有效载荷部分(14),具有有效载荷整流罩(16)和中央部分(18),其包括有效载荷(20)和布置在有效载荷(20)之后并与之连接的有效载荷推进单元(22)有效载荷(20)。为了防止或分别限制相互的相对运动,有效载荷整流罩(16)和中心部分(18)通过连接装置连接,该连接装置附接到有效载荷整流罩(16)并且还可释放地连接到中心(18)。该连接装置实施为优选为扁平的壳体(24),该壳体可以由两个部分壳体(24.1、24.2)组成,所述两个局部壳体可释放地彼此固定。

著录项

  • 公开/公告号US6086020A

    专利类型

  • 公开/公告日2000-07-11

    原文格式PDF

  • 申请/专利权人 CONTRAVES SPACE AG;

    申请/专利号US19980105552

  • 发明设计人 MARIO MACHIUSSI;

    申请日1998-06-26

  • 分类号B64G1/00;

  • 国家 US

  • 入库时间 2022-08-22 01:36:44

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