The invention relates to an integrated heat dissipation structure of a low-
orbit satellite phased-array antenna, and relates to the technical field of
satellite heat dissipation. The integrated heat dissipation structure comprises a heat
storage area, a heat conductor and an aluminum
ammonia heat pipe which are arranged between a
satellite body and a phased-array antenna, one end of the aluminum
ammonia heat pipe is in contact with a heating device of the phased-array antenna, and the other end of the aluminum
ammonia heat pipe is inserted into the heat conductor; the heat
storage area is filled with a
phase change material used for absorbing and storing heat, one side of the heat
storage area is attached to a satellite body, and the other side of the heat storage area is attached to the heat conductor; the satellite body is further provided with a plurality of heat dissipation teeth used for dissipating heat in the heat storage area. Aiming at the characteristics that a low-
orbit satellite is small in ground winding period and short in starting time, through the heat dissipation structure which comprehensively covers conduction, heat storage and
radiation and is integrally designed, the heat dissipation requirement of the low-
orbit satellite phased-array antenna can be better met, and the heat dissipation performance and reliability of the satellite-borne digital phased-array antenna are improved.