FIELD: manufacturing technology.
SUBSTANCE: invention relates to large-sized deployed satellite antenna reflector. Peculiar feature of disclosed reflector is that assembly units are composed of elements in form of tetrahedron, connected to each other to form ring-shaped structure; wherein tetrahedrons have corresponding triangular bases, connected to each other on corresponding first sides axial ends and having corresponding external vertices, opposite to said corresponding first sides and when reflector is in open configuration, lying on elliptical cone, which tangents to parabolic mirror.
EFFECT: technical result is improved control over reflector deployment.
12 cl, 19 dwg
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Authors
Dates
2017-01-20—Published
2013-11-04—Filed