Systems, methods, and apparatuses for the direct mount of secondary payload adapters to a truss structure common to a space vehicle payload adapter are disclosed herein. In one or more embodiments, a method for reacting loads into a space vehicle payload adapter comprises reacting, by more than two interstitial rings of the space vehicle payload adapter, the loads created by secondary payloads mounted onto the space vehicle payload adapter, into a truss structure of the space vehicle payload adapter. The method further comprises reacting, by struts of the truss structure, the loads to a forward ring and an aft ring of the space vehicle payload adapter. In one or more embodiments, the reacting of the loads maintains high frequency (e.g., greater than (>) thirty (30) gigahertz (GHz)) modes for the space vehicle payload adapter.
DIRECT MOUNT OF SECONDARY PAYLOAD ADAPTERS TO TRUSS STRUCTURE COMMON TO SPACE VEHICLE PAYLOAD ADAPTER
DIREKTE BEFESTIGUNG VON SEKUNDÄRNUTZLASTADAPTERN AN EINER TRÄGERSTRUKTUR FÜR EINEN RAUMFAHRZEUGNUTZLASTADAPTER
MONTAGE DIRECT D'ADAPTATEURS DE CHARGE UTILE SECONDAIRE SUR UNE STRUCTURE EN TREILLIS COMMUNE À UN ADAPTATEUR DE CHARGE UTILE DE VÉHICULE SPATIAL
2024-05-29
Patent
Elektronische Ressource
Englisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Europäisches Patentamt | 2022
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|Truss structure for directly mounting secondary payload adapters to space craft payload adapters
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