FIELD: rocketry and space engineering. SUBSTANCE: compartment-platform has inner and outer load-bearing envelopes arranged one in other and connected together; envelopes are provided with end frames; compartment-platform is also provided with bearing brackets to receive transportation supports, rod members with attachment units for securing to frames of envelopes, attachment units for securing the payload components to compartment and attachment units for securing the compartment to rocket. Compartment platform is provided with adapter made in form of load-bearing envelope with end frames and panel with stiffeners, seats for payload components and attachment units for securing them to panel and for securing the panel to compartment. Panel has curvilinear outer contour embracing the adapter; panel is rigidly connected with front frames of load-bearing envelopes of compartment. Stiffeners of panel are located between seats of payload components and attachment units for securing it to frames of load-bearing envelopes. EFFECT: enhanced reliability. 13 cl, 6 dwg
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Authors
Dates
1997-02-10—Published
1993-06-09—Filed