A system includes a satellite structure and a dedicated Payload Attaching Fitting PAF for releasable attachment to said satellite structure. The satellite structure an external load-carrying structure; and external vertical planar panels. The external vertical planar panels have internal reinforcements or embedded structures or skin thickness reinforcements, each configured for exerting the structural reinforcement function of diagonal beams in a truss structure architecture.
EFFICIENT SATELLITE STRUCTURE CONCEPT FOR SINGLE OR STACKING MULTIPLE LAUNCHES
2021-07-22
Patent
Electronic Resource
English
IPC: | B64G Raumfahrt , COSMONAUTICS |
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