Modular spacecraft construction requiring no tools for assembly and disassembly
A modular spacecraft construction having a simple spacecraft core structure (10) of cylindrical shape, spacecraft equipment modules (12) in the form of generally flat panels that are attached in a radial configuration about the core structure, and electronic sub-modules (16) secured to the faces of...
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Main Authors | , |
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Format | Patent |
Language | English |
Published |
22.05.2001
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Edition | 7 |
Subjects | |
Online Access | Get full text |
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Summary: | A modular spacecraft construction having a simple spacecraft core structure (10) of cylindrical shape, spacecraft equipment modules (12) in the form of generally flat panels that are attached in a radial configuration about the core structure, and electronic sub-modules (16) secured to the faces of the spacecraft equipment modules. Hand-operated fasteners (14, 18) facilitate assembly of the modules (12) to the core structure (10) and of the electronic sub-modules (16) to the modules. Each spacecraft equipment module (12) is secured to the core structure (10) using multiple hook-type latches (14) that are hand-operated to secure the module to the core structure. Each sub-module (16) is secured to an equipment module (12) by fasteners (18) of a different type that are also hand-operated. These fasteners (18) have a one-way ratchet a mechanism that prevents their deliberate or inadvertent loosening. |
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Bibliography: | Application Number: US19980204775 |