FIELD: aviation.
SUBSTANCE: modular space vehicle (SV) includes onboard equipment box, one of the boxes contains the SV service equipment, and the other box contains the target equipment and sensors of the control system command and control instruments. The target equipment unit is integrated with the service system unit via three hinged supports. The service system unit is attached to the system of separation through the plate, and there are three hinges between the service system unit body and the fixing plate to the separation system. The basis of the service system unit power structure is a triangular prism, hinges are located in the corners of its bases. The SV separation system is attached to the carrier rocket upper-stage rocket transitional farm at three points, lying on the rays - continuations of the lateral edges of the power prism.
EFFECT: ensured minimization of mechanical stress caused by thermal expansion and narrowing in the bodies of space vehicle modules.
5 cl, 3 dwg
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Authors
Dates
2017-05-31—Published
2015-12-31—Filed