FIELD: transport.
SUBSTANCE: invention relates to space and missile equipment and can be used for final carrier rocket stages. A space and missile system (SMS) includes a carrier rocket with a final stage with an outer housing compartment with an intermediate power support frame with outer and inner frames connected to each other by means of fastening elements; a space vehicle with the main fairing with an end frame. The outer diameter of the intermediate support power frame corresponds to the diameter of the end frame of the main fairing.
EFFECT: invention allows attachment of different standard sizes of main fairings with carrier rockets without increasing the time for assembly and preparation for SMS launching.
2 dwg
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Authors
Dates
2015-07-10—Published
2013-09-12—Filed