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    Modular spacecraft design
    13.
    发明公开
    Modular spacecraft design 有权
    航天器的模块化结构

    公开(公告)号：EP1101699A3

    公开(公告)日：2003-12-03

    申请号：EP00203766.1

    申请日：2000-10-27

    申请人： The Boeing Company

    发明人： Loosli, Bruce Glen ,  Gerhardt, David Lee ,  Weiss, Courtney Ross

    IPC分类号： B64G1/10 ,  B64G1/22 ,  B64G1/64

    CPC分类号： B64G1/10 ,  B64G1/22 ,  B64G1/64 ,  B64G2001/1092

    摘要： A spacecraft (10) comprised of a plurality of functionally organized, fully independent modules (12,14,16,18). Selected ones of the modules are moveable foldably in a "clamshell"-like manner between assembled positions, wherein various components of the spacecraft are generally not readily accessible, to a service position in which virtually all of the components of the spacecraft are substantially readily accessible for service or testing. Logically organized and routed harnesses (46,47,46') comprised of numerous electrical and mechanical elements (24-38) enable the clamshell-like folding movement of selected modules. Conventional electrical and mechanical connectors (48) associated with the harnesses permit quick detachment and complete removal of selected modules from the spacecraft. The fully modular design significantly reduces the time required to gain access to the components on each of the modules and eliminates time consuming and extensive disassembly procedures that would ordinarily be required when performing service or test procedures on the spacecraft. The fully modular configuration also permits parallel manufacturing and testing of the independent modules, thus significantly reducing the design-to-market cycle time for the spacecraft. The modular design also facilitates replacement of selected modules with modified modules to produce derivative spacecraft or to tailor the performance of the spacecraft to better meet the needs of a particular mission.

    Nutzlastträger für Raumstationen
    15.
    发明公开
    Nutzlastträger für Raumstationen 有权
    NutzlastträgerfürRaumstationen

    公开(公告)号：EP1022219A2

    公开(公告)日：2000-07-26

    申请号：EP99125594.4

    申请日：1999-12-22

    申请人： DaimlerChrysler Aerospace AG

    发明人： Bank, Christian, Dipl.-Ing.

    IPC分类号： B64G1/22 ,  B64G1/12

    CPC分类号： B64G1/22 ,  B64G1/12 ,  B64G1/641

    摘要： Ein Nutzlastträger für Raumstationen besteht aus einer Gitterstruktur, die mit einer ersten, als Anschlußpunkt an die Raumstation ausgebildeten Außenfläche auf eine an der Raumstation angeordnete, mit Versorgungsanschlüssen versehene und als Nahtstelle ausgebildete Aufnahmeeinheit aufsetzbar ist, wobei diese Außenfläche ein zur Nahtstelle passendes Kopplungselement aufweist. Weitere Außenflächen der Gitterstruktur sind ihrerseits als Aufnahmeeinheiten entweder für weitere Nutzlastträger oder für aktive bzw. passive Nutzlasten ausgebildet.

    摘要翻译： 有用的负载载体具有开放的栅格结构（11），其具有作为到空间站的连接点的第一外表面（12,13）和与接收单元相对应的耦合元件。 网格结构的至少一个外表面被设计为接收单元（14-19），其中至少一个具有具有供应连接的接缝部分。

    Spacecraft module with embedded heaters and sensors, and related method of manufacture
    18.
    发明公开
    Spacecraft module with embedded heaters and sensors, and related method of manufacture 审中-公开
    航天器模块具有嵌入的加热元件和传感器和相关联的制造过程

    公开(公告)号：EP1004507A2

    公开(公告)日：2000-05-31

    申请号：EP99122038.5

    申请日：1999-11-15

    申请人： TRW INC.

    发明人： Anderson, Joseph F.

    IPC分类号： B64G1/22 ,  B64G1/66 ,  B64G1/50

    CPC分类号： B64G1/66 ,  B64G1/22 ,  B64G1/50 ,  B64G7/00 ,  B64G2001/1092

    摘要： A technique for reducing the cost of manufacturing spacecraft, wherein many resistive heaters (14), and sensors (20) such as thermistors and strain gauges are integrated into a spacecraft equipment module (10 or 12) during fabrication. Prior to testing, selected heaters (14) and sensors (20) are activated through external connectors (18) to the equipment module (10 or 12). Prior to launch of the spacecraft, selected heaters and sensors needed during flight are activated and the heaters and sensors needed for test are deactivated.

    摘要翻译： 一种用于减少制造航天器的成本，worin许多电阻加热器制造（14）和传感器（20）的技术：如热敏电阻和应变计被集成到航天器设备模块（10或12）中。 在测试之前，加热器选择（14）和传感器（20）通过外部连接器（18）到所述设备模块（10或12）激活。 发射宇宙飞船之前，在飞行过程中需要选择的加热器和传感器被激活并需要测试的加热器和传感器是失活的。

    DISPOSITIF DE SUSPENSION D'UNE CHARGE UTILE DANS UN LANCEUR SPATIAL
    19.
    发明公开
    DISPOSITIF DE SUSPENSION D'UNE CHARGE UTILE DANS UN LANCEUR SPATIAL 失效
    设备的有效载荷的在运载火箭吊

    公开(公告)号：EP0956236A1

    公开(公告)日：1999-11-17

    申请号：EP98905458.0

    申请日：1998-01-29

    申请人： CENTRE NATIONAL D'ETUDES SPATIALES

    发明人： HUBERT, Pascal, Marie-Dominique

    IPC分类号： B64G1 ,  F16F1 ,  F16F9

    CPC分类号： F16F1/54 ,  B64G1/22 ,  B64G1/641 ,  F16F9/0418 ,  F16F9/10

    摘要： The invention concerns a device for the suspension of a payload in a space launch comprising annular chambers of fluid with variable geometry (12i) installed between said launch and said payload and first (10') and second (11') rigid members fixed, on either side of said chambers (12i), to said payload and to the launch respectively so as to transmit the stresses between the latter through said chambers. The fluid chambers (12i) and the first (10') and second (11') rigid coupling members are coextensive, ring-shaped and coaxial with a longitudinal axis common to the launch and to the payload. The first (10') and second (11') annular rigid coupling members each comprise external (10a', 10b') and internal (11a', 11b') ribs respectively, axially separated by one of the annular fluid chamber (12i).