FIELD: space transport equipment.
SUBSTANCE: adapter includes body rigidly fixed to launching platform; power supply system and power supply distribution and control system located inside body and connected with power supply source. There is at least one interface module for interaction with auxiliary work load carried by the carrier rocket. Other modules of subsystems (data storage, sensor and data interfaces, communication means) can be envisaged for the purpose of specific auxiliary work load and/or its flight programme. Adapter does not interact with stage of main work load. It can be modified providing only functional capabilities required for the given auxiliary work load.
EFFECT: reduction of costs for space delivery of new developed spacecraft with maintenance of integrity and improvement of operational reliability for traditional space delivery system of working loads.
11 cl, 4 dwg
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