ANTI-AIRCRAFT GUIDED MISSILE 9M96E2 Russian patent published in 2023 - IPC F42B15/00 

FIELD: ammunition.

SUBSTANCE: missile contains a body, an engine placed in it, equipment for a guidance and control system, an on-board transponder (4), steering mechanisms, a homing head (2), a non-contact fuse (5), a safety actuator (6), combat equipment and a power source , interconnected by electrical bundles, it is configured to be placed in a sealed transport and launch container (TLC), with an external connector (10) connected to a detachable connector (8) of the rocket to ensure the exchange of starting information between the ground equipment of the launch automation and the rocket's computing environment, uniting digital computers (DCs) of components and blocks of the rocket. The onboard equipment of the rocket additional includes the board (12) for exchange of program information. The outputs of the non-volatile memory microcircuits of the DCs of the components and blocks of the rocket, intended for rewriting the information of the DC software, are output to the external connector (10) of the corresponding node or block. Additional lines (11), (13) and (14) for information exchange are introduced into the composition of the rocket electrical bundles, one of which (13) connects the external connectors (10) of the nodes and blocks of the rocket, to which the outputs of the microcircuits of the non-volatile memory of the DC with the board (12) for exchange of program information, and the other line (14) connects the board (12) for exchange of program information with the detachable connector (8) of the missile and through it with the external connector of the TLC (10).

EFFECT: possibility to flash new software into the DC of components and blocks without rolling out the rocket from the TLC and disassembling it into component nodes and blocks.

1 cl, 1 dwg