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A cylindrical satellite, a stack of cylindrical satellites, and a launching device for such a satellite

机译:圆柱卫星,一堆圆柱卫星以及用于这种卫星的发射装置

摘要

The satellite (1) is composed of a cylindrical main body (2). The inner wall (3) of the main body (2) is divided into an inner space (9) and an outer wall (4), and is extended by a main axis, from the lowest (5) area to the uppermost (6) area, Including the lowest surface (5) of an interface device (7) in cooperation with a carrier rocket supplementary interface device (20), including a satellite (1),In addition, there is at least one internal device (10) installed in the main internal wall (3) (2), and at least partially extended to the internal space (9), and the main external wall (4) comprises at least a part (19) of a flat surface, forming a side, The built-in device (10) includes an optical view instrument and an electronic instrument associated with the optical instrument (13), including an optical instrument (13), an optical axis (V) and a view axis (2) parallel to the main axis (a),The satellite (1) is characterized in that at least one external panel (15) is fixed on the outer wall (4) of the main body, and the external panel (15) is horizontally projected on the outer wall (4) of the main shaft (a), It is at least an external device (15), either a propulsion tank or an inertial driver, such as a gyroscope driver or a reaction wheel, and the external device (15) is fixed on at least a flat surface part (19) to form a side surface.
机译:卫星(1)由圆柱形主体(2)组成。主体(2)的内壁(3)被分为内部空间(9)和外壁(4),并且沿主轴线从最低(5)区域延伸到最高(6)。 )区域,包括接口装置(7)的最低表面(5)与运载火箭辅助接口装置(20)配合使用,包括卫星(1),此外,至少有一个内部装置(10)安装在主内壁(3)(2)中,并至少部分地延伸到内部空间(9),并且主外壁(4)包括至少一部分平面(19),形成侧面内置装置(10)包括光学观察仪器和与该光学仪器(13)相关联的电子仪器,该电子仪器包括光学仪器(13),与之平行的光轴(V)和观察轴(2)。卫星(1)的特征在于,至少一个外部面板(15)固定在主体的外壁(4)上,并且外部面板(15)是水平的。在主轴(a)的外壁(4)上呈放射状地突出,至少是外部装置(15),该外部装置是推进箱或惯性驱动器,例如陀螺仪驱动器或反作用轮,以及外部装置(15)至少固定在平坦的表面部分(19)上以形成侧面。

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