The invention discloses a truss structure for directly mounting a secondary payload adapter to a space craft payload adapter. Systems, methods, and apparatus for mounting secondary payload adapters directly to a truss structure common to space craft payload adapters. In one or more embodiments, a method of counteracting a load to a space craft payload adapter includes passing through more than two spacer rings of the space craft payload adapter, a load generated by a secondary payload mounted on the space craft payload adapter is counteracted into a truss structure of the space craft payload adapter. The method further includes counteracting the load to the front ring and the rear ring of the space craft payload adapter through the struts of the truss structure. In one or more embodiments, the reaction of the load maintains a high frequency (e.g., greater than (gt; ) a thirty (30) Gilz (GHz) mode.
本文公开了将二级有效载荷适配器直接安装到太空飞行器有效载荷适配器通用的桁架结构。用于将二级有效载荷适配器直接安装到太空飞行器有效载荷适配器共有的桁架结构的系统、方法和装置。在一个或多个实施例中,将载荷反作用到太空飞行器有效载荷适配器的方法包括通过太空飞行器有效载荷适配器的多于两个间隙环,将由安装在太空飞行器有效载荷适配器上的二级有效载荷产生的载荷反作用到太空飞行器有效载荷适配器的桁架结构中。该方法还包括:通过桁架结构的支柱,将载荷反作用到太空飞行器有效载荷适配器的前环和后环。在一个或多个实施例中,载荷的反作用为太空飞行器有效载荷适配器保持高频(例如,大于(>)三十(30)吉赫(GHz))模式。
Truss structure for directly mounting secondary payload adapters to space craft payload adapters
将二级有效载荷适配器直接安装到太空飞行器有效载荷适配器通用的桁架结构
2022-08-05
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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