FIELD: astronautics.
SUBSTANCE: invention relates mainly to housing elements of small spacecrafts (MCA), made using new technologies from sandwich-panels (SP) based on foamed aluminum. SP can be used for adhesive bonding of foam with aluminum covers. For SP assembly, attachments are used, which are added on surface of SP by additive (3D) method. At the same time from the SP surface the cover section is removed, the section similar to the remote one is formed by 3D-method, and the bracket of the required configuration is made on it. Then, formed unit is connected with SP.
EFFECT: technical result is simplification of MCA creation technology with achievement of high mass-strength, protective and damping characteristics.
1 cl, 6 dwg
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