METHOD OF PAYLOAD INTEGRATION AND DEVICE TO THIS END Russian patent published in 2016 - IPC B64G1/00 

FIELD: transport.

SUBSTANCE: invention relates to space engineering and can be used for spacecraft payload integration. Claimed device comprises the spacecraft and is composed of the separable structural tube of isogrid to make the spacecraft load-bearing body. It consists of the parts depending on the height and quantity of spacecraft in the payload, with constant cross-section area within one part and cross-section increasing toward the carrier rocket adapter. Spacecraft are built around appropriate units of separable parts of said detachable load-bearing tube at the Manufacturers' to combine said spacecraft to the integral payload. The spacecraft head is assembled to include the payload and nose cowling. Now, said head is mounted at its prescribed seat at carrier rocket.

EFFECT: compact design, ease of assembly.

5 cl, 2 dwg