GUIDED MISSILE Russian patent published in 1998 - IPC

FIELD: rocket weaponry. SUBSTANCE: body of missile houses control elements, power supply unit with thermoelectric cells and gyroscope. Case of power supply unit is fabricated in the form of clip from material with high thermal conductivity and has sockets where thermoelectric cells and gyroscope are installed. Cells are installed in sockets without clearance and are uniformly arranged around socket with gyroscope. Guaranteed clearance exists between clip and body of missile in zone of placement of cells. EFFECT: increased accuracy and stability of operation of guided missile at low temperatures thanks to heating up of gyroscope by heat released with functioning of missile. 3 dwg