FIELD: physics.
SUBSTANCE: invention relates to the structural elements of payloads (PL), in particular, microsatellites. Adapter includes a farm with two tiers of triangular lattices: the upper tier is made in the form of a cylinder, and the lower one is in the form of a truncated cone. The support nodes (4, 8) form the upper and lower belts. The layers are joined through the support units of the intermediate belt. The first means (10) for fastening passing MD (41) contain boxes in the form of boxes. Their bottom panels can be provided with projections for the installation of control units (42) by the separation of the MD (41). The second securing means (20) of associated MD (41) comprise a framework in the form of a straight triangular prism fixed to the lower tier of the truss. The securing means (10, 20) allow the separation of the MD (41) in the lateral direction relative to the axis (40).
EFFECT: reducing the weight of the adapter to remove a significant number of microsatellites of the Kubsat class, in the presence of a point joint of the adapter with the accelerating unit and the main payload.
5 cl, 17 dwg
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Authors
Dates
2017-07-11—Published
2016-04-28—Filed