FIELD: astronautics.
SUBSTANCE: invention relates to space engineering, particularly, to transient compartments of carrier rockets and their trusses. Transient compartment of carrier rocket comprises housing and spacer fitted therein and provided with payload attachment device. Transient compartment comprises second payload attachment device made in the form of spatial truss with triangular grid. Upper ends of rods of spatial truss are rigidly connected to each other by fittings made with possibility of attachment to payload at distance from spacer main frame and separation from payload. Lower ends of rods of spatial truss are pivotally connected to support units fixed on transverse and longitudinal beams of transition compartment. Support units of the spatial truss are made so that they can turn the truss rods to the acute angle and fix them in the turned position after separation of the truss fittings from the payload.
EFFECT: enabling increase in useful volume.
17 cl, 27 dwg
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Authors
Dates
2019-08-14—Published
2018-11-15—Filed