FIELD: space technology.
SUBSTANCE: invention relates to the field of space technology and can be used in the manufacture of spacecraft. The spacecraft assembly method includes installation of supporting panel structures on the central part of the spacecraft in the + YОZ and -YОZ planes. On these structures, vertical honeycomb panels are fixed, located parallel to the XOZ plane. Each of the vertical honeycomb panels is connected to the service systems module and the base panel of the payload module. The base panel is located in the YOZ plane. Support and instrument panels are located in the + XOZ and –XOZ planes.
EFFECT: increased rigidity of the spacecraft.
1 cl, 2 dwg
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